Index (ORbit Extrapolation KIT 6.1 API)

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

A

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final semi major axis.
a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: a.
A - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: A = sqrt(μ * a).
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original recovered semi major axis.
AbsoluteDate - Class in org.orekit.time: This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate: Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive: Parameter name for absorption coefficient.
AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical: Common handling of Propagator methods for analytical propagators.
AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Build a new instance.
AbstractDetector - Class in org.orekit.propagation.events: Common parts shared by several orbital events finders.
AbstractDetector(double, double) - Constructor for class org.orekit.propagation.events.AbstractDetector: Deprecated.
as of 6.1, replaced with AbstractDetector.AbstractDetector(double, double, int)
AbstractDetector(double, double, int) - Constructor for class org.orekit.propagation.events.AbstractDetector: Build a new instance.
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces: Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Build a new instance.
AbstractIntegratedPropagator - Class in org.orekit.propagation.integration: Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator: Build a new instance.
AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration: Differential equations for the main state (orbit, attitude and mass).
AbstractPropagator - Class in org.orekit.propagation: Common handling of Propagator methods for analytical propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator: Build a new instance.
AbstractPropagatorConverter - Class in org.orekit.propagation.conversion: Common handling of PropagatorConverter methods for propagators conversions.
AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter: Build a new instance.
AbstractReconfigurableDetector<T extends EventDetector> - Class in org.orekit.propagation.events: Builder reconfiguration API for detectors.
AbstractReconfigurableDetector(double, double, int, EventHandler<T>) - Constructor for class org.orekit.propagation.events.AbstractReconfigurableDetector: Build a new instance.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.drag.DragForce: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.drag.DragForce: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in interface org.orekit.forces.ForceModel: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in interface org.orekit.forces.ForceModel: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.OceanTides: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.OceanTides: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.SolidTides: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.SolidTides: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Compute acceleration derivatives with respect to state parameters.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Compute acceleration derivatives with respect to additional parameters.
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.propagation.numerical.Jacobianizer: Compute acceleration and derivatives with respect to state.
accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.propagation.numerical.Jacobianizer: Compute acceleration and derivatives with respect to parameter.
acceptStep(AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Accept a step, triggering events and step handlers.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder: Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder: Build a new instance.
AdapterPropagator - Class in org.orekit.propagation.analytical: Orbit propagator that adapts an underlying propagator, adding differential effects.
AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator: Build a propagator from an underlying reference propagator.
AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical: Interface for orbit differential effects.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer: Add a step handler.
addAcceleration(Vector3D, Frame) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of an acceleration expressed in some inertial frame.
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState: Add an additional state.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator: Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator: Add a set of user-specified state parameters to be computed along with the orbit propagation.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory: Add a loader for celestial bodies.
addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame: Add a child.
addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame: Add a child.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.drag.DragForce: Compute the contribution of the drag to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.OceanTides: Compute the contribution of the force model to the perturbing acceleration.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Add the contribution of the wave to Stokes coefficients.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.SolidTides: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Compute the contribution of the force model to the perturbing acceleration.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, String, String, String) - Static method in class org.orekit.frames.FramesFactory: Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String) - Static method in class org.orekit.frames.FramesFactory: Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Add the default READERS for ocean tides.
addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Add the default readers for gravity fields.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager: Add the default providers configuration.
addDefaultUTCTAILoader() - Static method in class org.orekit.time.TimeScalesFactory: Add the default loader for UTC-TAI offsets history files.
addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Add a differential effect.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Static method in class org.orekit.frames.FramesFactory: Add a loader for Earth Orientation Parameters history.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector: Add an event date.
addEventDetector(T) - Method in class org.orekit.propagation.AbstractPropagator: Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator: Add an event detector.
addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Add a force model to the global perturbation model.
AdditionalEquations - Interface in org.orekit.propagation.integration: This interface allows users to add their own differential equations to a numerical propagator.
AdditionalStateProvider - Interface in org.orekit.propagation: This interface represents providers for additional state data beyond SpacecraftState.
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of the Kepler evolution.
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of the flow rate (dm/dt).
addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Add a reader for ocean tides.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Add an offset from the instance.
addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic: Add a fitting point.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Add a reader for gravity fields.
addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager: Add a data provider to the supported list.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3File: Add a new satellite with a given identifier to the list of stored satellites.
addSatelliteCoordinate(String, SatelliteTimeCoordinate) - Method in class org.orekit.files.sp3.SP3File: Adds a new P/V coordinate for a given satellite.
addSwitchingCondition(AttitudeProvider, T, boolean, boolean, AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence: Add a switching condition between two attitude providers.
addUTCTAILoader(UTCTAILoader) - Static method in class org.orekit.time.TimeScalesFactory: Add a loader for UTC-TAI offsets history files.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Add parsed coefficients.
addXYZAcceleration(double, double, double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of an acceleration expressed in the inertial frame (it is important to make sure this acceleration is defined in the same frame as the orbit) .
afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Method called just after integration.
AlignmentDetector - Class in org.orekit.propagation.events: Finder for satellite/body alignment events.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Build a new alignment detector.
AltitudeDetector - Class in org.orekit.propagation.events: Finder for satellite altitude crossing events.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AngularCoordinates - Class in org.orekit.utils: Simple container for rotation/rotation rate pairs.
AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates: Simple constructor.
AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates: Builds a rotation/rotation rate pair.
ApparentElevationDetector - Class in org.orekit.propagation.events: Deprecated.
as of 6.1 replaced by ElevationDetector
ApparentElevationDetector(double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Build a new apparent elevation detector.
ApparentElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Build a new apparent elevation detector.
ApparentElevationDetector(double, double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Build a new apparent elevation detector.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect: Apply the effect to a spacecraft state.
apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect: Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect: Apply the effect to a spacecraft state.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic: Approximate an already fitted model to polynomial only terms.
ApsideDetector - Class in org.orekit.propagation.events: Finder for apside crossing events.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector: Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector: Build a new instance.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants: Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential: Parser for tides astronomical amplitude H_f.
AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Simple constructor.
Atmosphere - Interface in org.orekit.forces.drag: Interface for atmospheric models.
AtmosphericRefractionModel - Interface in org.orekit.models: Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.
ATOMIC_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000: Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000: Identifier for atomic oxygen.
attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame: Attach the instance (and all its children down to leafs) to the main tree.
attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame: Attach the instance (and all its children down to leafs) to the main tree.
Attitude - Class in org.orekit.attitudes: This class handles attitude definition at a given date.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude: Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D) - Constructor for class org.orekit.attitudes.Attitude: Creates a new instance.
AttitudeProvider - Interface in org.orekit.attitudes: This interface represents an attitude provider model set.
AttitudeProviderModifier - Interface in org.orekit.attitudes: This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes: This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence: Constructor for an initially empty sequence.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction: Suffix for parameter name for attraction coefficient enabling jacobian processing.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities: Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Simple constructor.

B

B - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: B = sqrt(1 - h² - k²).
B_STAR - Static variable in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Parameter name for B* coefficient.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Propagate an orbit without any fancy features.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Method called just before integration.
BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants: Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.
beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: 1 - e2.
BodiesElements - Class in org.orekit.data: Elements of the bodies having an effect on nutation.
BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements: Simple constructor.
BodyCenterPointing - Class in org.orekit.attitudes: This class handles body center pointing attitude provider.
BodyCenterPointing(Frame) - Constructor for class org.orekit.attitudes.BodyCenterPointing: Creates new instance.
BodyShape - Interface in org.orekit.bodies: Interface representing the rigid surface shape of a natural body.
BoundedPropagator - Interface in org.orekit.propagation: This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces: experimental class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lightning of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lightning of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces: Class representing a single facet of a convex spacecraft body.
BoxAndSolarArraySpacecraft.Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Simple constructor.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in interface org.orekit.propagation.conversion.FirstOrderIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder: Build a first order integrator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder: Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Build a propagator.
buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a propagator.
buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Build a coefficients row.
buildTriangularArray(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Build a coefficients triangular array.
BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the BulletinB files (IAU1980 compatibles).
BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the BulletinB files (IAU2000 compatibles).

C

C - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: C = 1 + p² + q².
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: C1 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: C2 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: C4 from SPTRCK #3.
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential: Caching wrapper for NormalizedSphericalHarmonicsProvider.
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Simple constructor.
calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField: Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.
calculatePathDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
calculatePathDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
calculatePathDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericDelayModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
calculateSignalDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay: Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.
calculateSignalDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel: Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.
calculateSignalDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericDelayModel: Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Check if coefficients can be added.
CartesianOrbit - Class in org.orekit.orbits: This class holds cartesian orbital parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from cartesian parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from any kind of orbital parameters.
CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.
CCSDSFrame - Enum in org.orekit.files.ccsds: Frames used in CCSDS Orbit Data Messages.
CelestialBody - Interface in org.orekit.bodies: Interface for celestial bodies like Sun, Moon or solar system planets.
CelestialBodyFactory - Class in org.orekit.bodies: Factory class for bodies of the solar system.
CelestialBodyLoader - Interface in org.orekit.bodies: Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes: This class handles a celestial body pointed attitude provider.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed: Creates new instance.
CenterName - Enum in org.orekit.files.ccsds: Orbit central bodies for which a Celestial body can be created.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction: Name of the single parameter of this model: the central attraction coefficient.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory: Check Earth orientation parameters continuity.
ChronologicalComparator - Class in org.orekit.time: Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator: Simple constructor.
CircularFieldOfViewDetector - Class in org.orekit.propagation.events: Finder for target entry/exit events with respect to a satellite sensor Field Of View.
CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector: Build a new instance.
CircularOrbit - Class in org.orekit.orbits: This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance.
CircularOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Deprecated.
as of 6.0 replaced by CircularOrbit.CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from cartesian parameters.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from any kind of orbital parameters.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a new instance.
ClasspathCrawler - Class in org.orekit.data: Provider for data files stored as resources in the classpath.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler: Build a data classpath crawler.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler: Build a data classpath crawler.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear all loaded celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear loaders for all celestial bodies.
clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory: Clear loaders for Earth Orientation Parameters history.
clearEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator: Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator: Remove all events detectors.
clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager: Clear the set of data file names that have been loaded.
clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger: Clear the logged events.
clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Clear ocean tides readers.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Clear gravity field readers.
clearProviders() - Method in class org.orekit.data.DataProvidersManager: Remove all data providers.
clearUTCTAILoaders() - Static method in class org.orekit.time.TimeScalesFactory: Clear loaders for UTC-TAI offsets history files.
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: C / (2 * A * B) .
coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: coef for SGP C3 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: coef for SGP C5 computation.
CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities: This class is designed to provide coefficient from the DSST theory.
CoefficientsFactory.MNSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities: MNS couple's key.
CoefficientsFactory.MNSKey(int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey: Simpleconstructor.
CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities: Key formed by two integer values.
CoefficientsFactory.NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey: Simple constructor.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator: Compare two time-stamped instances.
compareTo(CoefficientsFactory.MNSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate: Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
compile(PoissonSeries<S>...) - Static method in class org.orekit.data.PoissonSeries: Join several nutation series, for fast simultaneous evaluation.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations: Compute differential equations for main state.
computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations: Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Compute the derivatives related to the additional state parameters.
computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory: Compute recursively G_s and H_s polynomials from equation 3.1-(5).
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame: Compute the limit visibility point for a satellite in a given direction.
computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory: Compute the Q_n,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory: Compute the V_n,s coefficients from 2.8.2-(1)(2).
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Configure ocean load deformation coefficients.
Constants - Interface in org.orekit.utils: Set of useful physical constants.
ConstantThrustManeuver - Class in org.orekit.forces.maneuvers: This class implements a simple maneuver with constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver: Simple constructor for a constant direction and constant thrust.
containsSatellite(String) - Method in class org.orekit.files.ccsds.ODMFile: Tests whether a satellite with the given id is contained in this orbit file.
containsSatellite(String) - Method in interface org.orekit.files.general.OrbitFile: Tests whether a satellite with the given id is contained in this orbit file.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3File: Tests whether a satellite with the given id is contained in this orbit file.
ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Event handler which will always return continue as a state.
ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter: Convert a row.
convert(Propagator, double, int, Collection<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Convert a propagator to another.
convert(List<SpacecraftState>, boolean, Collection<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter: Convert an osculating orbit into a mean orbit, in DSST sense.
convert(Propagator, double, int, Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Convert a propagator into another one.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Convert a propagator into another one.
convert(List<SpacecraftState>, boolean, Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert(EventDetector.Action) - Static method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Conversion between pre-6.1 EventDetector.Action and post-6.1 EventHandler.Action.
convert(EventHandler.Action) - Static method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Conversion between post 6.1 EventHandler.Action and pre-6.1 EventDetector.Action.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the instance type.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: cosinus original inclination.
create(double, double, int, EventHandler<ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Build a new instance.
create(double, double, int, EventHandler<T>) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Build a new instance.
create(double, double, int, EventHandler<AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector: Build a new instance.
create(double, double, int, EventHandler<AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector: Build a new instance.
create(double, double, int, EventHandler<ApparentElevationDetector>) - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Build a new instance.
create(double, double, int, EventHandler<ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector: Build a new instance.
create(double, double, int, EventHandler<CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Build a new instance.
create(double, double, int, EventHandler<DateDetector>) - Method in class org.orekit.propagation.events.DateDetector: Build a new instance.
create(double, double, int, EventHandler<DihedralFieldOfViewDetector>) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Build a new instance.
create(double, double, int, EventHandler<EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector: Build a new instance.
create(double, double, int, EventHandler<ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector: Build a new instance.
create(double, double, int, EventHandler<EventFilter<T>>) - Method in class org.orekit.propagation.events.EventFilter: Build a new instance.
create(double, double, int, EventHandler<EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter: Build a new instance.
create(double, double, int, EventHandler<GroundMaskElevationDetector>) - Method in class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Build a new instance.
create(double, double, int, EventHandler<NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector: Build a new instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Besselian Epoch (BE).
createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents: Build a date from week components.
createGPSDate(int, double) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a GPS date.
createIllegalArgumentException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException: Create an IllegalArgumentException with localized message.
createIllegalStateException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException: Create an IllegalStateException with localized message.
createInternalError(Throwable) - Static method in exception org.orekit.errors.OrekitException: Create an RuntimeException for an internal error.
createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Julian Epoch (JE).
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a mapper between raw double components and spacecraft state.
createParseException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException: Create an ParseException with localized message.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined: Create an ITRF frame by transforming another ITRF frame.
CunninghamAttractionModel - Class in org.orekit.forces.gravity: This class represents the gravitational field of a celestial body.
CunninghamAttractionModel(Frame, double, double, double[][], double[][]) - Constructor for class org.orekit.forces.gravity.CunninghamAttractionModel: Deprecated.
since 6.0, replaced by CunninghamAttractionModel.CunninghamAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider)
CunninghamAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.CunninghamAttractionModel: Creates a new instance.

D

DataLoader - Interface in org.orekit.data: Interface for loading data files from data providers.
DataProvider - Interface in org.orekit.data: Interface for providing data files to file loaders.
DataProvidersManager - Class in org.orekit.data: Singleton class managing all supported data providers.
DateComponents - Class in org.orekit.time: Class representing a date broken up as year, month and day components.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its components.
DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its components.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents: Build a date from a year and day number.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents: Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events: Finder for date events.
DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance.
DateTimeComponents - Class in org.orekit.time: Holder for date and time components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents: Build a new instance from its components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from a seconds offset with respect to another one.
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache: Default number of independent cached time slots.
DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Default correction factor value.
DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader: Default supported files name pattern for JPL DE files.
DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader: Default supported files name pattern for IMCCE INPOP files.
DEFAULT_LAW - Static variable in interface org.orekit.propagation.Propagator: Default attitude provider.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator: Default mass.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector: Default cmaximum number of iterations in the event time search.
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector: Default maximum checking interval (s).
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides: Default number of points tides field sampling.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides: Default number of points tides field sampling.
DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Default local pressure at viewpoint (Pa).
DEFAULT_PRESSURE - Static variable in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Default local pressure at viewpoint (Pa).
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides: Default step for tides field sampling (seconds).
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides: Default step for tides field sampling (seconds).
DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Default local temperature at viewpoint (K).
DEFAULT_TEMPERATURE - Static variable in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Default local temperature at viewpoint (K).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector: Default convergence threshold (s).
DelaunayArguments - Class in org.orekit.data: Delaunay arguments used for nutation or tides.
DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments: Simple constructor.
DihedralFieldOfViewDetector - Class in org.orekit.propagation.events: Finder for body entering/exiting dihedral FOV events.
DihedralFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, Vector3D, double, Vector3D, double) - Constructor for class org.orekit.propagation.events.DihedralFieldOfViewDetector: Build a new instance.
DirectoryCrawler - Class in org.orekit.data: Provider for data files stored in a directories tree on filesystem.
DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler: Build a data files crawler.
DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for DormandPrince54Integrator.
DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder: Build a new instance.
DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for DormandPrince853Integrator.
DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder: Build a new instance.
DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive: Parameter name for drag coefficient enabling jacobian processing.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to drag, with state derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in interface org.orekit.forces.drag.DragSensitive: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in interface org.orekit.forces.drag.DragSensitive: Compute the acceleration due to drag, with state derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in interface org.orekit.forces.drag.DragSensitive: Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.SphericalSpacecraft: Compute the acceleration due to drag, with state derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in class org.orekit.forces.SphericalSpacecraft: Compute acceleration due to drag, with parameters derivatives.
DragForce - Class in org.orekit.forces.drag: Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce: Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag: Interface for spacecraft that are sensitive to atmospheric drag forces.
DrozinerAttractionModel - Class in org.orekit.forces.gravity: This class represents the gravitational field of a celestial body.
DrozinerAttractionModel(Frame, double, double, double[][], double[][]) - Constructor for class org.orekit.forces.gravity.DrozinerAttractionModel: Deprecated.
since 6.0, replaced by DrozinerAttractionModel.DrozinerAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider)
DrozinerAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.DrozinerAttractionModel: Creates a new instance.
dsEvaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions: Evaluate the date offset between the current date and the reference date.
DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces: Atmospheric drag contribution to the DSSTPropagator.
DSSTAtmosphericDrag(Atmosphere, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Simple constructor.
DSSTCentralBody - Class in org.orekit.propagation.semianalytical.dsst.forces: Central body gravitational contribution to the DSSTPropagator.
DSSTCentralBody(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: DSST Central body constructor.
DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces: This interface represents a force modifying spacecraft motion for a DSSTPropagator.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst: This class propagates orbits using the DSST theory.
DSSTPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a new instance of DSSTPropagator.
DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces: Solar radiation pressure contribution to the DSSTPropagator.
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Simple constructor with default reference values.
DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Complete constructor.
DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces: Third body attraction perturbation to the DSSTPropagator.
DSSTThirdBody(CelestialBody) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Complete constructor.
DTM2000 - Class in org.orekit.forces.drag: This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.DTM2000: Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.forces.drag: Container for solar activity data, compatible with DTM2000 Atmosphere model.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate: Compute the physically elapsed duration between two instants.

E

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final eccentricity.
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original eccentricity squared.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Earth.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Earth-Moon barycenter.
EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth: Implementation of refraction model for Earth standard atmosphere.
EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Creates a new default instance.
EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Creates an instance given a specific pressure and temperature.
ecc - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Eccentricity.
ECCENTRIC_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
ECCENTRIC_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
ECCENTRIC_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical: This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Private helper constructor.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, mass and potential provider.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EcksteinHechlerPropagatorBuilder(Frame, double, double, TideSystem, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EclipseDetector - Class in org.orekit.propagation.events: Finder for satellite eclipse related events.
EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector: Deprecated.
as of 6.1 replaced by EclipseDetector.EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) followed by either a call to EclipseDetector.withUmbra() or by a call to EclipseDetector.withPenumbra()
EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector: Deprecated.
as of 6.1 replaced by EclipseDetector.EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) followed by either a call to EclipseDetector.withUmbra() or by a call to EclipseDetector.withPenumbra()
EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector: Deprecated.
as of 6.1 replaced by EclipseDetector.EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) followed by either a call to EclipseDetector.withUmbra() or by a call to EclipseDetector.withPenumbra()
EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original eccentricity * eta.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for EGM files.
EGMFormatReader - Class in org.orekit.forces.gravity.potential: This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader: Simple constructor.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².
ElevationDetector - Class in org.orekit.propagation.events: Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector: Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
ElevationDetector(double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector: Deprecated.
as of 6.1 replace with ElevationDetector.ElevationDetector(TopocentricFrame) followed by a call to ElevationDetector.withConstantElevation(double)
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector: Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationMask - Class in org.orekit.utils: Class for modeling the ground elevation values around a given point.
ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask: Creates an instance of an Elevation mask based on the passed in parameter.
EME2000_ALIGNED - Static variable in class org.orekit.attitudes.InertialProvider: Dummy attitude provider, perfectly aligned with the EME2000 frame.
emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache: Get an empty immutable cache, cast to the correct type.
endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: End parsing.
ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState: Check if two instances have the same set of additional states available.
EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the EOPC04 files (IAU1980 compatibles).
EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the EOPC04 files (IAU2000 compatibles).
EOPEntry - Class in org.orekit.frames: This class holds an Earth Orientation Parameters entry.
EOPEntry(int, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.EOPEntry: Simple constructor.
EOPHistory - Class in org.orekit.frames: This class loads any kind of Earth Orientation Parameter data throughout a large time range.
EOPHistory(IERSConventions, Collection<EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory: Simple constructor.
EOPHistoryLoader - Interface in org.orekit.frames: Interface for loading Earth Orientation Parameters history.
Ephemeris - Class in org.orekit.propagation.analytical: This class is designed to accept and handle tabulated orbital entries.
Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator: Indicator for ephemeris generation mode.
equals(Object) - Method in class org.orekit.bodies.GeodeticPoint
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
equals(Object) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represent the same time as another instance.
equals(Object) - Method in class org.orekit.time.DateComponents
equals(Object) - Method in class org.orekit.time.DateTimeComponents
equals(Object) - Method in class org.orekit.time.TimeComponents
EquinoctialOrbit - Class in org.orekit.orbits: This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance.
EquinoctialOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Deprecated.
as of 6.0 replaced by EquinoctialOrbit.EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from cartesian parameters.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from any kind of orbital parameters.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates: Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates: Estimate FieldRotation rate between two orientations.
estimateSpin(Rotation, Rotation, double) - Static method in class org.orekit.attitudes.Attitude: Deprecated.
as of 6.0 superseded by AngularCoordinates.estimateRate(Rotation, Rotation, double)
estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates: Estimate velocity between two positions.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates: Estimate velocity between two positions.
eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: eta from SPTRCK #3.
etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: eta squared.
EulerIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for EulerIntegrator.
EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder: Build a new instance.
evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments: Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateDerivative(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments: Evaluate all fundamental arguments for the current date (Delaunay plus planetary), including the first time derivative.
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState: Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions: Evaluate the date offset between the current date and the reference date.
EventDetector - Interface in org.orekit.propagation.events: This interface represents space-dynamics aware events detectors.
EventDetector.Action - Enum in org.orekit.propagation.events: Deprecated.
as of 6.1, replaced with EventHandler.Action
EventFilter<T extends EventDetector> - Class in org.orekit.propagation.events: Wrapper used to detect only increasing or decreasing events.
EventFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventFilter: Wrap an event detector.
EventHandler<T extends EventDetector> - Interface in org.orekit.propagation.events.handlers: An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
EventHandler.Action - Enum in org.orekit.propagation.events.handlers: Enumerate for actions to be performed when an event occurs.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector: Deprecated.
as of 6.1 replaced by EventHandler.eventOccurred(SpacecraftState, EventDetector, boolean)
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Deprecated.
as of 6.1 replaced by EventHandler.eventOccurred(SpacecraftState, EventDetector, boolean)
eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector: Deprecated.
as of 6.1 replaced by EventHandler.eventOccurred(SpacecraftState, EventDetector, boolean)
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler: eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing: Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing: Handle a detection event and choose what to do next.
EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events: Wrapper shifting events occurrences times.
EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter: Build a new instance.
EventsLogger - Class in org.orekit.propagation.events: This class logs events detectors events during propagation.
EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger: Simple constructor.
EventsLogger.LoggedEvent - Class in org.orekit.propagation.events: Class for logged events entries.
EventState<T extends EventDetector> - Class in org.orekit.propagation.events: This class handles the state for one event detector during integration steps.
EventState(T) - Constructor for class org.orekit.propagation.events.EventState: Simple constructor.
extendListOfLists(List<List<Double>>, int, int, double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Extend a list of lists of coefficients if needed.

F

f - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Equinoctial frame f vector.
FactoryManagedFrame - Class in org.orekit.frames: Base class for the predefined frames that are managed by FramesFactory.
FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame: Simple constructor.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler: Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in interface org.orekit.data.DataProvider: Feed a data file loader by browsing the data collection.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager: Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler: Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.NetworkCrawler: Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ZipJarCrawler: Feed a data file loader by browsing the data collection.
FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for FES C hat and epsilon tides files.
FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for FES Cnm, Snm tides files.
FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for FES Hf tides files.
FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential: Reader for ocean tides files following the fes2004.dat format.
FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader: Simple constructor.
FESCnmSnmReader - Class in org.orekit.forces.gravity.potential: Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.
FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader: Simple constructor.
FieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils: Simple container for FieldRotation/FieldRotation rate pairs, using RealFieldElement.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Builds a FieldRotation/FieldRotation rate pair.
FieldBodiesElements<T extends RealFieldElement<T>> - Class in org.orekit.data: Elements of the bodies having an effect on nutation.
FieldBodiesElements(AbsoluteDate, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements: Simple constructor.
FieldDelaunayArguments<T extends RealFieldElement<T>> - Class in org.orekit.data: Delaunay arguments used for nutation or tides.
FieldDelaunayArguments(AbsoluteDate, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments: Simple constructor.
FieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils: Simple container for Position/Velocity pairs, using RealFieldElement.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a PVCoordinates pair.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Subtractive constructor
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for 1950 dates: 1950-01-01.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader: Load celestial body.
FilterType - Enum in org.orekit.propagation.events: Enumerate for filtering events.
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion: Propagator converter using finite differences to compute the jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Simple constructor.
FirstOrderIntegratorBuilder - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction to build first order integrators for propagators conversion.
fit() - Method in class org.orekit.utils.SecularAndHarmonic: Fit parameters.
FixedRate - Class in org.orekit.attitudes: This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate: Creates a new instance.
FixedTransformProvider - Class in org.orekit.frames: Transform provider using fixed transform.
FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider: Simple constructor.
FixedTroposphericDelay - Class in org.orekit.models.earth: A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.
FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the DataProvidersManager.
ForceModel - Interface in org.orekit.forces: This interface represents a force modifying spacecraft motion.
Frame - Class in org.orekit.frames: Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame: Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame: Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors: This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException: Simple constructor.
FramesFactory - Class in org.orekit.frames: Factory for predefined reference frames.
freeze() - Method in class org.orekit.frames.Transform: Get a freezed transform.
FundamentalNutationArguments - Class in org.orekit.data: Class computing the fundamental arguments for nutation and tides.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate: Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventFilter: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector: Compute the value of the switching function.
g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Equinoctial frame g vector.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants: Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for Galileo System Time: 1999-08-22.
GalileoScale - Class in org.orekit.time: Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the Γ^m_n,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(double[], double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Simple constructor.
generate(T, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator: Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile: Generate a CartesianOrbit from the KeplerianOrbit.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile: Generate a CartesianOrbit from the OPM state vector data.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile: Generate a KeplerianOrbit based on the OMM mean keplerian elements.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OPMFile: Generate a KeplerianOrbit from the OPM keplerian elements if hasKeplerianElements is true, or from the state vector data otherwise.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.OMMFile: Generate spacecraft state from the KeplerianOrbit generated by generateKeplerianOrbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.OPMFile: Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateTLE() - Method in class org.orekit.files.ccsds.OMMFile: Generate TLE from OMM file.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils: Generic thread-safe cache for time-stamped data.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>, Class<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache: Simple constructor.
GeodeticPoint - Class in org.orekit.bodies: Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint: Build a new instance.
GeoMagneticElements - Class in org.orekit.models.earth: Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements: Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth: Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField: Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth: Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth: The currently supported geomagnetic field models.
GeoMagneticModelLoader - Class in org.orekit.models.earth: Loads geomagnetic field models from a given input stream.
GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters: Get the last 24H mean geomagnetic index.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: The Kp index is derived from the Ap index.
getA() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit semi-major axis.
getA() - Method in class org.orekit.orbits.CartesianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit: Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState: Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the abscissa grid for the interpolation function.
getAbsorptionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get the absorption coefficient.
getAbsorptionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive: Get the absorption coefficient.
getAbsorptionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft: Get the absorption coefficient.
getAcceleration() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesDataLine: Get the ephemerides data line acceleration vector.
getAcceleration(SpacecraftState, Vector3D, Vector3D) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Compute the acceleration due to the non conservative perturbing force.
getAcceleration(SpacecraftState, Vector3D, Vector3D) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Compute the acceleration due to the non conservative perturbing force.
getAcceleration(SpacecraftState, Vector3D, Vector3D) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Compute the acceleration due to the non conservative perturbing force.
getAccuracy() - Method in class org.orekit.files.general.SatelliteInformation: Returns the estimated accuracy of the orbit entries for this satellite (in m).
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the adapted propagator.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider: Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState: Get an additional state.
getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper: Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator: Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState: Get an unmodifiable map of additional states.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the value of the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider: Deprecated.

Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.ProviderConverter: Deprecated.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the value of the central body reference radius.
getAgency() - Method in class org.orekit.files.sp3.SP3File: Returns the agency that prepared this SP3 file.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get all of the data in this cache.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine α for central body.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric latitude argument.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit: Get the mean latitude argument.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit: Get the true latitude argument.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector: Get the threshold altitude value.
getAncestor(int) - Method in class org.orekit.frames.Frame: Get the n^th ancestor of the frame.
getAngular() - Method in class org.orekit.frames.Transform: Get the underlying elementary angular part.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates: Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates: Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit: Get the anomaly.
getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile: Get the type of anomaly (true or mean).
getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the Geomagnetic planetary 3-hour index A_p.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Get facet area.
getArea() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the cross sectional area of satellite.
getArea() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the cross sectional area of satellite.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the atmospheric model.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingWrapper: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider: Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState: Get the attitude.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator: Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper: Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator: Get attitude provider.
getAvailableParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the available free parameters.
getAvailableParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Get the names of the available parameters in the propagator.
getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the available satellite numbers.
getAxis1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Get the direction of FOV 1st dihedral axis.
getAxis2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Get the direction of FOV 2nd dihedral axis.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the azimuth of a point with regards to the topocentric frame center point.
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get B = sqrt(1 - e²).
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingWrapper: Compute the base system state at given date, without compensation.
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get state vector dimension without additional parameters.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine β for central body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Get a celestial body.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing: Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape: Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the body frame related to body shape.
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector: Get the body shape.
getBStar() - Method in class org.orekit.files.ccsds.OMMFile: Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the ballistic coefficient.
getC(int, int, boolean) - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider: Deprecated.

Get the tesseral-sectorial and zonal coefficients.
getC(int, int, boolean) - Method in class org.orekit.forces.gravity.potential.ProviderConverter: Deprecated.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get C = 1 + p² + q².
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration: Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents: Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month: Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month: Get the capitalized full name.
getCartesian() - Method in class org.orekit.frames.Transform: Get the underlying elementary cartesian part.
getCd() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the drag coefficient.
getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName: Get the celestial body corresponding to the CCSDS constant.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Get the direction of FOV center.
getCenter() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Get the direction of FOV center.
getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the CelestialBody corresponding to the center name.
getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the origin of reference frame.
getChildren() - Method in class org.orekit.frames.OrphanFrame: Get all children of the instance.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the circular eccentricity vector.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the CIRF2000 reference frame.
getCIRF2000(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
since 6.1 repaced with FramesFactory.getCIRF(IERSConventions, boolean)
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile: Get the classification type.
getClockCorrection() - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Returns the clock correction value.
getClockRateChange() - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Returns the clock rate change value.
getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the closest TLE to the selected date.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients: Get the load deformation coefficients for ocean tides.
getComment() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the meta-data comment.
getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get the maneuvers data comment, each string in the list corresponds to one line of comment.
getCompensation(PVCoordinatesProvider, AbsoluteDate, Frame, Attitude) - Method in class org.orekit.attitudes.GroundPointingWrapper: Compute the compensation rotation at given date.
getCompensation(PVCoordinatesProvider, AbsoluteDate, Frame, Attitude) - Method in class org.orekit.attitudes.YawCompensation: Compute the compensation rotation at given date.
getCompensation(PVCoordinatesProvider, AbsoluteDate, Frame, Attitude) - Method in class org.orekit.attitudes.YawSteering: Compute the compensation rotation at given date.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the constant gravity field coefficients provider from the first supported file.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get a time-independent provider for read spherical harmonics coefficients.
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the constant gravity field coefficients provider from the first supported file.
getConventions() - Method in class org.orekit.files.ccsds.ODMFile: Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ODMParser: Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory: Get the IERS conventions to which these EOP apply.
getCoordinate() - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Returns the coordinate of this entry.
getCoordinateSystem() - Method in class org.orekit.files.ccsds.OEMFile: Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in class org.orekit.files.ccsds.OMMFile: Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in class org.orekit.files.ccsds.OPMFile: Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in interface org.orekit.files.general.OrbitFile: Returns the coordinate system of the entries in this orbit file.
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File: Returns the coordinate system of the entries in this orbit file.
getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for covariance.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the list of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile: Get the Position/Velocity covariance matrix.
getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile: Get coordinate system for covariance matrix, for absolute frames.
getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile: Get coordinate system for covariance matrix, for Local Orbital Frames.
getCr() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the satellite radiation pressure coefficient (assuming total specular reflection).
getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile: Get the file creation date and time in UTC.
getCurrentDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the current grid date.
getD() - Method in class org.orekit.data.DelaunayArguments: Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean elongation of the Moon from the Sun.
getDataUsed() - Method in class org.orekit.files.sp3.SP3File: Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude: Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments: Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments: Get the date.
getDate() - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry: Get the date.
getDate() - Method in class org.orekit.frames.Transform: Get the date.
getDate() - Method in class org.orekit.orbits.Orbit: Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the TLE current date.
getDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the date of the initial state.
getDate() - Method in class org.orekit.propagation.events.DateDetector: Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState: Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate: Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents: Get the date component.
getDate() - Method in interface org.orekit.time.TimeStamped: Get the date.
getDay() - Method in class org.orekit.time.DateComponents: Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3File: Returns the day fraction for this SP3 file.
getDayOfWeek() - Method in class org.orekit.time.DateComponents: Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents: Get the day number in year.
getDdEps() - Method in class org.orekit.frames.EOPEntry: Get the correction for nutation in obliquity δΔε.
getDdPsi() - Method in class org.orekit.frames.EOPEntry: Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField: Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the declination of the magnetic field in degrees.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the decreasing events time shift.
getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay: Returns the default model, loading delay values from the file "tropospheric-delay.txt".
getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get mass change during maneuver (value is < 0).
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere: Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.DTM2000: Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000: Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.HarrisPriester: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.HarrisPriester: Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.JB2006: Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere: Get the local density.
getDepth() - Method in class org.orekit.frames.Frame: Get the depth of the frame.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Get Γ function derivative.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_α coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_β coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_h coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_k coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_α coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_β coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_h coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_k coefficient.
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value D_n^l(Χ).
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the Doodson number for the wave.
getDragArea() - Method in class org.orekit.files.ccsds.OGMFile: Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile: Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get the drag coefficient.
getDragCoefficient() - Method in interface org.orekit.forces.drag.DragSensitive: Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft: Get the drag coefficient.
getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get duration (value is 0 for impulsive maneuver).
getDUT1(AbsoluteDate) - Method in class org.orekit.frames.TidalCorrection: Deprecated.

Get the dUT1 value.
getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get velocity increment.
getDx() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit eccentricity.
getE() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit: Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState: Get the eccentricity.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache: Get the earliest entry in this cache.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Earth singleton body.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Earth-Moon barycenter singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame: Get the east direction of topocentric frame, expressed in parent shape frame.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric anomaly.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the differential effects.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the element number.
getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile: Get the element set number for this satellite.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the elevation of a point with regards to the local point.
getElevation() - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Get the threshold apparent elevation value.
getElevation(double) - Method in class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Get the interpolated elevation for a given azimuth according to the mask.
getElevation(double) - Method in class org.orekit.utils.ElevationMask: Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured elevation mask.
getEME2000() - Static method in class org.orekit.frames.FramesFactory: Get the unique EME2000 frame.
getEndDate() - Method in class org.orekit.frames.EOPHistory: Get the date of the last available Earth Orientation Parameters.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the total number of entries cached.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.time.UT1Scale: Get the EOP history.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions: Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile: Get the list of ephemerides blocks as an unmodifiable list.
getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the list of Ephemerides data lines.
getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the ephemerides data lines comment.
getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile: Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get the epoch relative to the covariance matrix.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile: Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.files.ccsds.OGMFile: Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in interface org.orekit.files.general.OrbitFile: Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Returns the epoch for this coordinate.
getEpoch() - Method in class org.orekit.files.sp3.SP3File: Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation: Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField: Returns the epoch for this magnetic field model.
getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for epoch.
getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.ccsds.ODMFile: Not supported by CCSDS orbit messages.
getEpochInterval() - Method in interface org.orekit.files.general.OrbitFile: Returns the time interval between epochs (in seconds).
getEpochInterval() - Method in class org.orekit.files.sp3.SP3File: Returns the time interval between epochs (in seconds).
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState: Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState: Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for equinox-based paradigm.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the number of objective function evaluations.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState: Get the underlying event detector.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce: There are no discrete events for this model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.CunninghamAttractionModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get the discrete events related to the model.
getEventTime() - Method in class org.orekit.propagation.events.EventState: Get the occurrence time of the event triggered in the current step.
getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper: Get the wrapped exception.
getExosphericTemp() - Method in class org.orekit.forces.drag.JB2006: Get the exospheric temperature above input position.
getF() - Method in class org.orekit.data.DelaunayArguments: Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments: Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).
getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame: Get the key of the frame within the factory.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the GeoMagneticField for the given model type and year.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the magnetic field vector in nTesla.
getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Get the date of the file from which data at the specified date comes from.
getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the first TLE.
getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the start date of the series.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the first known leap second.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic: Get a copy of the last fitted parameters.
getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator: Get the fixed step size.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the flattening of the body: f = (a-b)/a.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the flow rate.
getForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get perturbing force models list.
getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile: Get the CCSDS ODM (OPM, OMM or OEM) format version.
getFrame() - Method in interface org.orekit.bodies.CelestialBody: Deprecated.
as of 6.0 replaced by CelestialBody.getInertiallyOrientedFrame()
getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame: Get the frame corresponding to the CCSDS constant.
getFrame() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get coordinate system for covariance matrix, for absolute frames.
getFrame() - Method in interface org.orekit.forces.drag.Atmosphere: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.DTM2000: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.HarrisPriester: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.JB2006: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere: Get the frame of the central body.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory: Get one of the predefined frames.
getFrame() - Method in class org.orekit.frames.OrphanFrame: Get the associated frame.
getFrame() - Method in class org.orekit.orbits.Orbit: Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the frame of the initial state.
getFrame() - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector: Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
getFrame() - Method in class org.orekit.propagation.integration.StateMapper: Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState: Get the inertial frame.
getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData: Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData: Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFreeParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the free parameters.
getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame: Get a new version of the instance, frozen with respect to a reference frame.
getGamma() - Method in class org.orekit.data.DelaunayArguments: Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments: Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine γ for central body.
getGAST(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Deprecated.
as of 6.1, replaced by IERSConventions.getGASTFunction(org.orekit.time.TimeScale, EOPHistory)
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Static method in class org.orekit.frames.FramesFactory: Get the unique GCRF frame.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator: Get the ephemeris generated during propagation.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the generator.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGM() - Method in interface org.orekit.bodies.CelestialBody: Get the attraction coefficient of the body.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the G_ms^j coefficient.
getGMST(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Deprecated.
as of 6.1, replaced by IERSConventions.getGMSTFunction(org.orekit.time.TimeScale)
getGMST() - Static method in class org.orekit.time.TimeScalesFactory: Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich mean sidereal time, in radians.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory: Get the Global Positioning System scale.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3File: Returns the GPS week as contained in the SP3 file.
getGradient() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian: Get a reference to the gradient.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the number of interpolation grid points.
getGroundPointingLaw() - Method in class org.orekit.attitudes.GroundPointingWrapper: Deprecated.
as of 6.0, replaced by GroundPointingWrapper.getUnderlyingAttitudeProvider()
getGST() - Static method in class org.orekit.time.TimeScalesFactory: Get the Galileo System Time scale.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the GTOD reference frame.
getGTOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced with FramesFactory.getGTOD(IERSConventions, boolean)
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Get FOV half aperture angle.
getHalfAperture1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Get the half aperture angle of FOV 1st dihedra.
getHalfAperture2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Get the half aperture angle of FOV 2nd dihedra.
getHandler() - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Get the handler.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic: Get an upper bound of the fitted harmonic amplitude.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData: Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodyFactory.
getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile: Get boolean testing whether the OPM contains at least one maneuver.
getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get boolean testing whether the reference frame has an epoch associated to it.
getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile: Get the header comment.
getHessian() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian: Get a reference to the Hessian.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the H_ms^j coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHour() - Method in class org.orekit.time.TimeComponents: Get the hour number.
getHP() - Method in class org.orekit.propagation.numerical.ParameterConfiguration: Get parameter step.
getHx() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.SpacecraftState: Get the first component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.SpacecraftState: Get the second component of the inclination vector (as per equinoctial parameters).
getI() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit: Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState: Get the inclination.
getICRF() - Static method in class org.orekit.frames.FramesFactory: Get the unique ICRF frame.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the IGRF model for the given year.
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the inclination of the magnetic field in degrees.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the increasing events time shift.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get an inertially oriented, body centered frame.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator: Get the propagator initial state.
getInstance() - Static method in class org.orekit.data.DataProvidersManager: Get the unique instance.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters: Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Get the value of the instantaneous solar flux.
getInterpolatedDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the interpolated date.
getInterpolatedState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the interpolated state.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the interpolation method to be used.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getInverse() - Method in class org.orekit.frames.Transform: Get the inverse transform of the instance.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the specific impulse.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the ITRF2008 reference frame, using IERS 2010 conventions.
getITRF2000() - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_2000
getITRF2000(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_2000
getITRF2005() - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_2005
getITRF2005(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_2005
getITRF2008() - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced with FramesFactory.getITRF(IERSConventions, boolean)
getITRF2008(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced with FramesFactory.getITRF(IERSConventions, boolean)
getITRF93() - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_93
getITRF93(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_93
getITRF97() - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_97
getITRF97(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced by FramesFactory.getITRF(IERSConventions, boolean) and HelmertTransformation.Predefined.ITRF_2008_TO_ITRF_97
getITRFEquinox() - Static method in class org.orekit.frames.FramesFactory: Deprecated.
since 6.1 replaced with FramesFactory.getITRFEquinox(IERSConventions, boolean)
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the equinox-based ITRF reference frame.
getJ(boolean, int) - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider: Deprecated.

Get the zonal coefficients.
getJ(boolean, int) - Method in class org.orekit.forces.gravity.potential.ProviderConverter: Deprecated.
getJ2000Day() - Method in class org.orekit.time.DateComponents: Get the day number with respect to J2000 epoch.
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(double[][]) - Method in class org.orekit.frames.Transform: Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.CartesianOrbit
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJulianDay() - Method in class org.orekit.files.sp3.SP3File: Returns the julian day for this SP3 file.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Jupiter singleton body.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the x component of eccentricity vector.
getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for Keplerian elements.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit: Get the keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState: Get the keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit: Get the keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState: Get the keplerian period.
getL() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument.
getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the last TLE.
getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the last date of the series.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the last known leap second.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
getLatest() - Method in interface org.orekit.utils.TimeStampedCache: Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the latitude.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser: Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser: Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser: Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch year.
getLE() - Method in class org.orekit.data.BodiesElements: Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.SpacecraftState: Get the eccentric latitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Get the value of the previous leap.
getLightningRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lightning ratio ([0-1]).
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the second line.
getLJu() - Method in class org.orekit.data.BodiesElements: Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Jupiter longitude.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState: Get the mean latitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements: Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mars longitude.
getLMe() - Method in class org.orekit.data.BodiesElements: Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mercury longitude.
getLNe() - Method in class org.orekit.data.BodiesElements: Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Neptune longitude.
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager: Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocalTemp() - Method in class org.orekit.forces.drag.JB2006: Get the temperature at input position.
getLOD() - Method in class org.orekit.frames.EOPEntry: Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame: Get the type of Local Orbital frame.
getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get coordinate system for covariance matrix, for Local Orbital Frames.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger: Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the longitude.
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions: Get the Love numbers.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month: Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month: Get the lower case full name.
getLPrime() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Sun.
getLSa() - Method in class org.orekit.data.BodiesElements: Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Saturn longitude.
getLUr() - Method in class org.orekit.data.BodiesElements: Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Uranus longitude.
getLv() - Method in class org.orekit.orbits.CartesianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit: Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.SpacecraftState: Get the true latitude argument (as per equinoctial parameters).
getLVe() - Method in class org.orekit.data.BodiesElements: Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Venus longitude.
getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the differential equations to integrate (for main state only).
getMam() - Method in class org.orekit.forces.drag.DTM2000: Get the local mean atomic mass.
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator: Get all the names of all managed states.
getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile: Get a maneuver.
getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile: Get a list of all maneuvers.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mars singleton body.
getMass() - Method in class org.orekit.files.ccsds.OGMFile: Get the spacecraft mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState: Gets the current mass.
getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get the covariance matrix.
getMaxAlt() - Method in class org.orekit.forces.drag.HarrisPriester: Get the maximal altitude for the model.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector: Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get the maximal chunks duration.
getMaxDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the maximal supported degree.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector: Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the maximal supported order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the order limit for the next file parsing.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum number of independent cached time slots.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum duration span in seconds of one slot.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean anomaly.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData: Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters: Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile: Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile: Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile: Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing mean obliquity of the ecliptic.
getMEME(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.0, replaced by FramesFactory.getMOD(IERSConventions)
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mercury singleton body.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the meta-data for the block.
getMetaData() - Method in class org.orekit.files.ccsds.OGMFile: Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OMMFile: Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OPMFile: Get the meta data.
getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile: Get the comment for meta-data.
getMinAlt() - Method in class org.orekit.forces.drag.HarrisPriester: Get the minimal altitude for the model.
getMinDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the first date of the range.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured minimum valid elevation value.
getMinute() - Method in class org.orekit.time.TimeComponents: Get the minute number.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMFile: Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMParser: Get initial date.
getMjd() - Method in class org.orekit.frames.EOPEntry: Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.DateComponents: Get the modified julian day.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Get the MOD reference frame.
getMode() - Method in class org.orekit.propagation.AbstractPropagator: Get the current operating mode of the propagator.
getMode() - Method in interface org.orekit.propagation.Propagator: Get the current operating mode of the propagator.
getModelName() - Method in class org.orekit.models.earth.GeoMagneticField: Returns the model name.
getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader: Returns a Collection of the GeoMagneticField models that have been successfully loaded.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates: Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents: Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month: Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents: Get the month as an enumerate.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Moon singleton body.
getMu() - Method in class org.orekit.files.ccsds.ODMParser: Get gravitational coefficient.
getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider: Deprecated.

Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.ProviderConverter: Deprecated.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.Orbit: Get the central acceleration constant.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the Earth gravity coefficient used for TLE propagation.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the central body attraction coefficient.
getMu() - Method in class org.orekit.propagation.SpacecraftState: Get the central attraction coefficient.
getMuCreated() - Method in class org.orekit.files.ccsds.ODMFile: Get the gravitational coefficient created from the knowledge of the central body.
getMuParsed() - Method in class org.orekit.files.ccsds.ODMFile: Get the gravitational coefficient parsed in the ODM File.
getMuSet() - Method in class org.orekit.files.ccsds.ODMFile: Get the gravitational coefficient set by the user.
getMuUsed() - Method in class org.orekit.files.ccsds.ODMFile: Get the used gravitational coefficient.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey: Get n.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame: Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody: Get the name of the body.
getName() - Method in class org.orekit.frames.Frame: Get the name.
getName() - Method in enum org.orekit.frames.Predefined: Get the name of the frame.
getName() - Method in interface org.orekit.propagation.AdditionalStateProvider: Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations: Get the name of the additional state.
getName() - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the name of the partial Jacobians.
getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Get the name of the additional state.
getName() - Method in class org.orekit.time.GalileoScale: Get the name time scale.
getName() - Method in class org.orekit.time.GMSTScale: Get the name time scale.
getName() - Method in class org.orekit.time.GPSScale: Get the name time scale.
getName() - Method in class org.orekit.time.TAIScale: Get the name time scale.
getName() - Method in class org.orekit.time.TCBScale: Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale: Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale: Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale: Get the name time scale.
getName() - Method in class org.orekit.time.TTScale: Get the name time scale.
getName() - Method in class org.orekit.time.UT1Scale: Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale: Get the name time scale.
getNbManeuvers() - Method in class org.orekit.files.ccsds.OPMFile: Get the number of maneuvers present in the OPM.
getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache: Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache
getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache: Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Neptune singleton body.
getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache: Get quantum gap above which a new slot is created instead of extending an existing one.
getNewtonianAttractionForceModel() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get the Newtonian attraction from the central body force model.
getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory: Get the transform between two frames, suppressing all interpolation.
getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries: Get the number of different terms in the non-polynomial part.
getNonRotatingLaw() - Method in class org.orekit.attitudes.SpinStabilized: Deprecated.
as of 6.0, replaced by SpinStabilized.getUnderlyingAttitudeProvider()
getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNoradID() - Method in class org.orekit.files.ccsds.OMMFile: Get the NORAD Catalog Number ("Satellite Number").
getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Get unit normal vector.
getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get solar array normal in spacecraft frame.
getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get solar array normal in spacecraft frame.
getNormalizedCnm(double, int, int) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Deprecated.
getNormalizedCnm(double, int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider: Deprecated.
as of 6.1, replaced with NormalizedSphericalHarmonicsProvider.onDate(AbsoluteDate)
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics: Get a spherical harmonic cosine coefficient.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.
getNormalizedSnm(double, int, int) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Deprecated.
getNormalizedSnm(double, int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider: Deprecated.
as of 6.1, replaced with NormalizedSphericalHarmonicsProvider.onDate(AbsoluteDate)
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics: Get a spherical harmonic sine coefficient.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame: Get the north direction of topocentric frame, expressed in parent shape frame.
getNumber() - Method in enum org.orekit.time.Month: Get the month number.
getNumberOfEpochs() - Method in class org.orekit.files.ccsds.ODMFile: Not supported by CCSDS orbit messages.
getNumberOfEpochs() - Method in interface org.orekit.files.general.OrbitFile: Returns the number of epochs contained in this orbit file.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3File: Returns the number of epochs contained in this orbit file.
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions: Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing the nutation angles.
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions: Get the reference epoch for fundamental nutation arguments.
getObjectID() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the Jacobian of the function computing position/velocity at sample points.
getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Get the Jacobian of the function computing position/velocity at sample points.
getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter: Get the Jacobian of the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the spacecraft name for which the orbit state is provided.
getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector: Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector: Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector: Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector: Get the occulting body radius (m).
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the ocean tides waves from the first supported file.
getODMFile() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the ODM file to which these meta-data belong.
getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the offset from reference date for the harmonics.
getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the offset from reference date for the harmonics.
getOmega() - Method in class org.orekit.data.DelaunayArguments: Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean longitude of the ascending node of the Moon.
getOrbit() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesDataLine: Get the ephemerides data line orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState: Gets the current orbit.
getOrbitType() - Method in class org.orekit.files.sp3.SP3File: Returns the SP3File.SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get propagation parameter type.
getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the ordinate grid for the interpolation function.
getOrientation() - Method in class org.orekit.attitudes.Attitude: Get the complete orientation including spin.
getOriginator() - Method in class org.orekit.files.ccsds.ODMFile: Get the file originator.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the y component of inclination vector.
getPa() - Method in class org.orekit.data.BodiesElements: Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.data.FieldBodiesElements: Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit argument of pericenter.
getParameter(String) - Method in class org.orekit.forces.drag.DragForce
getParameter(String) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
getParameter(String) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
getParameter(String) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
getParameter(String) - Method in class org.orekit.forces.gravity.NewtonianAttraction
getParameter(String) - Method in class org.orekit.forces.gravity.OceanTides
getParameter(String) - Method in class org.orekit.forces.gravity.SolidTides
getParameter(String) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
getParameter(String) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
getParameter(String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
getParameter(String) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
getParameter(String) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
getParameter(String) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
getParameter(String) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
getParameterName() - Method in class org.orekit.propagation.numerical.ParameterConfiguration: Get parameter name.
getParameters() - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the number of parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get theJacobian with respect to parameters from a one-dimensional additional state array.
getParametersNames() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
getParent() - Method in class org.orekit.frames.Frame: Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame: Get the body shape on which the local point is defined.
getPartialDensities(int) - Method in class org.orekit.forces.drag.DTM2000: Get the local partial density of the selected element.
getParts() - Method in exception org.orekit.errors.OrekitException: Get the variable parts of the error message.
getPEF(boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.0, replaced by FramesFactory.getGTOD(IERSConventions, boolean)
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit: Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the argument of perigee.
getPermanentTide() - Method in enum org.orekit.utils.IERSConventions: Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the real part of a nominal Love numbers.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Pluto singleton body.
getPoint() - Method in class org.orekit.frames.TopocentricFrame: Get the surface point defining the origin of the frame.
getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole: Get the body North pole direction in ICRF frame.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the pole IERS Reference Pole correction.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.TidalCorrection: Deprecated.

Get the pole IERS Reference Pole correction.
getPolynomial() - Method in class org.orekit.data.PoissonSeries: Get the polynomial part of the series.
getPosition() - Method in class org.orekit.files.ccsds.OPMFile: Get position vector.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates: Gets the position.
getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get propagation parameter type.
getPotentialProvider() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Deprecated.
as of 6.0, replaced by GravityFieldFactory.getUnnormalizedProvider(int, int)
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing the precession angles.
getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Get the local pressure at the evaluation location.
getPressure() - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Get the local pressure at topocentric frame origin.
getPreviousDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the previous grid date.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole: Get the prime meridian angle.
getPropagator() - Method in class org.orekit.frames.SpacecraftFrame: Deprecated.

Get the underlying propagator.
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the reference propagator.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider() - Method in class org.orekit.propagation.numerical.ParameterConfiguration: Get the povider handling this parameter.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: Get the spherical harmonics provider.
getProviders() - Method in class org.orekit.data.DataProvidersManager: Get an unmodifiable view of the list of supported providers.
getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile: Get the position/velocity coordinates contained in the OPM.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.SpacecraftFrame: Deprecated.

Get the PVCoordinates of the spacecraft frame origin in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame: Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit: Get the PVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit: Get the PVCoordinates in definition frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries: Get the extrapolated position and velocity from an initial date.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState: Get the PVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState: Get the PVCoordinates in given output frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider: Get the PVCoordinates of the body in the selected frame.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the body to align.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get PV coordinates provider.
getPVTarget() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Get the position/velocity provider of the target .
getPVTarget() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector: Get the position/velocity provider of the target .
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the x component of inclination vector.
getRaan() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit right ascension of ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE: Get Right Ascension of the Ascending node.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the range of a point with regards to the topocentric frame center point.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the range rate of a point with regards to the topocentric frame center point.
getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics: Get a spherical harmonic cosine coefficient.
getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the underlying provider for raw (non-interpolated) transforms.
getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider: Get the position-velocity at date.
getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics: Get a spherical harmonic sine coefficient.
getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the critical distance.
getReal(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the real part of a nominal Love numbers.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate: Get the reference attitude.
getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the reference date for the harmonics.
getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the reference date for the harmonics.
getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper: Get reference date.
getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic: Get the reference date.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude: Get the reference frame.
getRefFrame() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get Coordinate system for velocity increment vector, for absolute frames.
getReflectionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get the specular reflection coefficient.
getReflectionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive: Get the specular reflection coefficient.
getReflectionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft: Get the specular reflection coefficient.
getRefLofType() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get coordinate system for velocity increment vector, for Local Orbital Frames.
getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel: Compute the refraction angle from the true (geometrical) elevation.
getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured refraction model.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the retrograde factor.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.OMMFile: Get the revolution rumber.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit: Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit: Get the right ascension of the ascending node.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the Root Mean Square Deviation of the fitting.
getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value R^ε_n,m,l(γ).
getRoot() - Static method in class org.orekit.frames.Frame: Get the unique root frame.
getRotation() - Method in class org.orekit.attitudes.Attitude: Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.Transform: Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the FieldRotation.
getRotationRate() - Method in class org.orekit.frames.Transform: Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the FieldRotation rate.
getS(int, int, boolean) - Method in interface org.orekit.forces.gravity.potential.PotentialCoefficientsProvider: Deprecated.

Get tesseral-sectorial coefficients.
getS(int, int, boolean) - Method in class org.orekit.forces.gravity.potential.ProviderConverter: Deprecated.
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey: Get s.
getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the EUV 81-day averaged centered index.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the states sample.
getSatellite(String) - Method in class org.orekit.files.ccsds.OEMFile: Get additional information about a satellite.
getSatellite(String) - Method in class org.orekit.files.ccsds.OGMFile: Get additional information about a satellite.
getSatellite(String) - Method in interface org.orekit.files.general.OrbitFile: Get additional information about a satellite.
getSatellite(String) - Method in class org.orekit.files.sp3.SP3File: Get additional information about a satellite.
getSatellite(int) - Method in class org.orekit.files.sp3.SP3File: Returns the nth satellite as contained in the SP3 file.
getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.ODMFile: Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.OEMFile: Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.OPMFile: Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in interface org.orekit.files.general.OrbitFile: Get the time coordinates for the given satellite.
getSatelliteCoordinates(String) - Method in class org.orekit.files.sp3.SP3File: Get the time coordinates for the given satellite.
getSatelliteCoordinatesOPM() - Method in class org.orekit.files.ccsds.OPMFile: Get the SatelliteTimeCoordinate of the OPM.
getSatelliteCount() - Method in class org.orekit.files.ccsds.OEMFile: Get the number of satellites contained in this orbit file.
getSatelliteCount() - Method in class org.orekit.files.ccsds.OGMFile: Get the number of satellites contained in this orbit file.
getSatelliteCount() - Method in interface org.orekit.files.general.OrbitFile: Get the number of satellites contained in this orbit file.
getSatelliteCount() - Method in class org.orekit.files.sp3.SP3File: Get the number of satellites contained in this orbit file.
getSatelliteId() - Method in class org.orekit.files.general.SatelliteInformation: Returns the id for this satellite object.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the satellite id.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.files.ccsds.OEMFile: Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSatellites() - Method in class org.orekit.files.ccsds.OGMFile: Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSatellites() - Method in interface org.orekit.files.general.OrbitFile: Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSatellites() - Method in class org.orekit.files.sp3.SP3File: Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Saturn singleton body.
getSecond() - Method in class org.orekit.time.TimeComponents: Get the seconds number.
getSecondsInDay() - Method in class org.orekit.time.TimeComponents: Get the second number within the day.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3File: Returns the seconds of the GPS week as contained in the SP3 file.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Computes the short periodic variations.
getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the short periodic variations.
getSize() - Method in class org.orekit.utils.LoveNumbers: Get the size of the arrays.
getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of slots in use.
getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of slots evictions.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the semi-major axis.
getSolarRadArea() - Method in class org.orekit.files.ccsds.OGMFile: Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.OGMFile: Get the solar radiation pressure coefficient.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the solar system barycenter aggregated body.
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSourceString() - Method in enum org.orekit.errors.OrekitMessages
getSouth() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame: Get the south direction of topocentric frame, expressed in parent shape frame.
getSpacecraftComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for spacecraft.
getSpecifier() - Method in exception org.orekit.errors.OrekitException: Get the localizable specifier of the error message.
getSpin() - Method in class org.orekit.attitudes.Attitude: Get the satellite spin.
getStandardModel() - Static method in class org.orekit.models.earth.SaastamoinenModel: Create a new Saastamoinen model using a standard atmosphere model.
getStartDate() - Method in class org.orekit.frames.EOPHistory: Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator: Get the start date.
getStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get start of total time span covered by ephemerides data and covariance data.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the triggering state.
getStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the state vector dimension.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the Jacobian with respect to state from a one-dimensional additional state array.
getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the grid points time step.
getStepHandler() - Method in class org.orekit.propagation.AbstractPropagator: Get the step handler.
getStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get end of total time span covered by ephemerides data and covariance data.
getStrengthLevel() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Get the strength level for activity.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Sun singleton body.
getSupportedNames() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Get the supported names for data files.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the regular expression for supported files names.
getSupportedNames() - Method in interface org.orekit.time.UTCTAILoader: Get the regular expression for supported UTC-TAI offsets files names.
getT() - Method in class org.orekit.forces.drag.DTM2000: Get the local temperature.
getTabDensity() - Method in class org.orekit.forces.drag.HarrisPriester: Get the current density table.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory: Get the International Atomic Time scale.
getTargetPoint(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing: Compute the target point in specified frame.
getTargetPoint(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the target point in specified frame.
getTargetPoint(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingWrapper: Compute the target point in specified frame.
getTargetPoint(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the target point in specified frame.
getTargetPoint(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute the target point in specified frame.
getTargetPoint(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing: Compute the target point in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingWrapper: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing: Compute the target point position/velocity in specified frame.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the size of the target.
getTC() - Method in class org.orekit.data.DelaunayArguments: Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments: Get the offset in Julian centuries.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory: Get the Barycentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory: Get the Geocentric Coordinate Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory: Get the Barycentric Dynamic Time scale.
getTEME() - Static method in class org.orekit.frames.FramesFactory: Get the TEME reference frame.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Get the local temperature at topocentric frame origin.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters: Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector: Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector: Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the thrust.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.CunninghamAttractionModel: Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel: Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the TideSystem used in the gravity field.
getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider: Get the TideSystem used in the gravity field.
getTime() - Method in class org.orekit.time.DateTimeComponents: Get the time component.
getTimeSystem() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.OEMFile: Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.files.ccsds.OMMFile: Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.files.ccsds.OPMFile: Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in interface org.orekit.files.general.OrbitFile: Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3File: Returns the OrbitFile.TimeSystem used to time-stamp position entries.
getTinf() - Method in class org.orekit.forces.drag.DTM2000: Get the current exospheric temperature above input position.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TIRF reference frame.
getTIRF2000(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
since 6.1 replaced with FramesFactory.getTIRF(IERSConventions)
getTIRF2000(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
since 6.1 replaced with FramesFactory.getTIRF(IERSConventions, boolean)
getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the underlying TLE.
getTLERelatedParametersComment() - Method in class org.orekit.files.ccsds.OMMFile: Get the comment for TLE related parameters.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TOD reference frame.
getTOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Deprecated.
as of 6.1, replaced with FramesFactory.getTOD(IERSConventions, boolean)
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TOD reference frame.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Get the topocentric frame.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Get the topocentric frame.
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector: Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the total intensity of the magnetic field (= norm of the field vector).
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Get the transform from TOD at specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation: Compute the transform at some date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider: Get the Transform corresponding to specified date.
getTransformProvider() - Method in class org.orekit.frames.Frame: Get the provider for transform from parent frame to instance.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame: Get the transform from the instance to another frame.
getTranslation() - Method in class org.orekit.frames.Transform: Get the underlying elementary translation.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the triggering event.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType: Get the increasing status of triggered events.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true anomaly.
getTT() - Static method in class org.orekit.time.TimeScalesFactory: Get the Terrestrial Time scale.
getType() - Method in class org.orekit.files.sp3.SP3File: Returns the SP3File.SP3FileType associated with this SP3 file.
getType() - Method in class org.orekit.orbits.CartesianOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.CircularOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.KeplerianOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.Orbit: Get the orbit type.
getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier: Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.GroundPointingWrapper: Get the underlying (ground pointing) attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized: Get the underlying attitude provider.
getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get a un-normalization factors array.
getUnnormalizedCnm(double, int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider: Deprecated.
as of 6.1, replaced with UnnormalizedSphericalHarmonicsProvider.onDate(AbsoluteDate)
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic cosine coefficient.
getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.
getUnnormalizedSnm(double, int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider: Deprecated.
as of 6.1, replaced with UnnormalizedSphericalHarmonicsProvider.onDate(AbsoluteDate)
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic sine coefficient.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month: Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month: Get the upper case full name.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Uranus singleton body.
getUseableStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUserDefinedParameters() - Method in class org.orekit.files.ccsds.OGMFile: Get the map of user defined parameter keywords and their corresponding values.
getUT1() - Static method in class org.orekit.time.TimeScalesFactory: Deprecated.
as of 6.1 replaced with TimeScalesFactory.getUT1(IERSConventions, boolean)
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory: Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory: Get the Universal Time 1 scale.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry: Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the UT1-UTC value.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory: Get the Universal Time Coordinate scale.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Get Γ function value.
getValue(int, int, int, DerivativeStructure) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials: Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators: Get the Newcomb operator evaluated at n, s, ρ, σ.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the values samples for the interpolation function.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get equinoctial frame vector w.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory: Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.files.ccsds.OPMFile: Get velocity vector.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere: Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000: Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.HarrisPriester: Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006: Get the inertial velocity of atmosphere molecules.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere: Get the inertial velocity of atmosphere molecules.
getVelocity() - Method in class org.orekit.frames.Transform: Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates: Gets the velocity.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Venus singleton body.
getVmns(int, int, int, double, double) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory: Get the V_n,s^m coefficient from V_n,s.
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the loaded waves.
getWest() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame: Get the west direction of topocentric frame, expressed in parent shape frame.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the WMM model for the given year.
getX() - Method in class org.orekit.frames.EOPEntry: Get the X component of the pole motion.
getXM10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters: Get the MG2 81-day average centered index.
getXp() - Method in class org.orekit.frames.PoleCorrection: Get the x_p parameter.
getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions: Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getY() - Method in class org.orekit.frames.EOPEntry: Get the Y component of the pole motion.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the yaw compensation angle at date.
getYear() - Method in class org.orekit.time.DateComponents: Get the year number.
getYp() - Method in class org.orekit.frames.PoleCorrection: Get the y_p parameter.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame: Get the zenith direction of topocentric frame, expressed in parent shape frame.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_ms^j and the H_ms^j polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Create a set of G_ms^j and H_ms^j polynomials.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder: Build a new instance.
GMSTScale - Class in org.orekit.time: Greenwich Mean Sidereal Time.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for GPS weeks: 1980-01-06.
GPSScale - Class in org.orekit.time: GPS time scale.
gradient(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute the gradient of the non-central part of the gravity field.
gradientHessian(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute both the gradient and the hessian of the non-central part of the gravity field.
GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for GraggBulirschStoerIntegrator.
GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder: Build a new instance.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential: Factory used to read gravity field files in several supported formats.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential: Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader: Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundMaskElevationDetector - Class in org.orekit.propagation.events: Deprecated.
as of 6.1 replaced by ElevationDetector
GroundMaskElevationDetector(double[][], TopocentricFrame) - Constructor for class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Build a new azimuth-elevation detector.
GroundMaskElevationDetector(double, double[][], TopocentricFrame) - Constructor for class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Build a new azimuth-elevation detector.
GroundMaskElevationDetector(double, double, double[][], TopocentricFrame) - Constructor for class org.orekit.propagation.events.GroundMaskElevationDetector: Deprecated.

Build a new azimuth-elevation detector.
GroundPointing - Class in org.orekit.attitudes: Base class for ground pointing attitude providers.
GroundPointing(Frame) - Constructor for class org.orekit.attitudes.GroundPointing: Default constructor.
GroundPointingWrapper - Class in org.orekit.attitudes: This class leverages common parts for compensation modes around ground pointing attitudes.
GroundPointingWrapper(GroundPointing) - Constructor for class org.orekit.attitudes.GroundPointingWrapper: Creates a new instance.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
GTODProvider - Class in org.orekit.frames: Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).
GTODProvider(IERSConventions, EOPHistory) - Constructor for class org.orekit.frames.GTODProvider: Simple constructor.
GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider: Pattern for name of gzip files.

H

h - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: e_y.
H00 - Static variable in class org.orekit.time.TimeComponents: Constant for commonly used hour 00:00:00.
H12 - Static variable in class org.orekit.time.TimeComponents: Constant for commonly used hour 12:00:00.
handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler: Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler: Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer: Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Handle the last accepted step.
HarrisPriester - Class in org.orekit.forces.drag: This atmosphere model is the realization of the Modified Harris-Priester model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.drag.HarrisPriester: Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.forces.drag.HarrisPriester: Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.forces.drag.HarrisPriester: Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.forces.drag.HarrisPriester: Constructor for Modified Harris-Priester atmosphere model.
hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState: Check if an additional state is available.
hasCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile: Check whether the OPM contains covariance matrix data.
hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().
hashCode() - Method in class org.orekit.bodies.GeodeticPoint
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
hashCode() - Method in class org.orekit.time.AbsoluteDate: Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.DateComponents
hashCode() - Method in class org.orekit.time.DateTimeComponents
hashCode() - Method in class org.orekit.time.TimeComponents
hasKeplerianElements() - Method in class org.orekit.files.ccsds.OGMFile: Check whether the OPM contains Keplerian elements data.
HELIUM - Static variable in class org.orekit.forces.drag.DTM2000: Identifier for helium.
HelmertTransformation - Class in org.orekit.frames: Transformation class for geodetic systems.
HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation: Build a transform from its primitive operations.
HelmertTransformation.Predefined - Enum in org.orekit.frames: Enumerate for predefined Helmert transformations.
HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for HighamHall54Integrator.
HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder: Build a new instance.
HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity: This class represents the gravitational field of a celestial body.
HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Creates a new instance.
HolmesFeatherstoneAttractionModel.GradientHessian - Class in org.orekit.forces.gravity: Container for gradient and Hessian.
HolmesFeatherstoneAttractionModel.GradientHessian(double[], double[][]) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian: Simple constructor.
HYDROGEN - Static variable in class org.orekit.forces.drag.DTM2000: Identifier for hydrogen.

I

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final inclination.
I - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Retrograde factor.
IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants: Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.
IAUPole - Interface in org.orekit.bodies: Interface for IAU pole and primer meridian orientations.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential: Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader: Simple constructor.
IDENTITY - Static variable in class org.orekit.frames.Transform: Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates: Fixed orientation parallel with reference frame (identity rotation and zero rotation rate).
IERSConventions - Enum in org.orekit.utils: Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils: Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils: A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache: Create a new cache with the given neighbors size and data.
ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers: Impulse maneuver model.
ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver: Build a new instance.
InertialProvider - Class in org.orekit.attitudes: This class handles an inertial attitude provider.
InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider: Creates new instance.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventFilter: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Initialize step handler at the start of a propagation.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Check if the initial state is provided in osculating elements.
initialize(boolean) - Method in interface org.orekit.propagation.integration.ModeHandler: Initialize the mode handler.
initialize(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody: Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Performs initialization at each integration step for the current force model.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Initialize the mapper.
initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.Orbit: Compute the position/velocity coordinates from the canonical parameters.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Check if date is within a leap second introduction.
IntegratedEphemeris - Class in org.orekit.propagation.integration: This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, ContinuousOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris: Creates a new instance of IntegratedEphemeris.
interpolate(AbsoluteDate, Collection<Attitude>) - Method in class org.orekit.attitudes.Attitude: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Transform>) - Method in class org.orekit.frames.Transform: Get an interpolated instance.
interpolate(AbsoluteDate, boolean, boolean, Collection<Transform>) - Static method in class org.orekit.frames.Transform: Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.CircularOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable: Get an interpolated instance.
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, AngularCoordinates>>) - Static method in class org.orekit.utils.AngularCoordinates: Interpolate angular coordinates.
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, FieldAngularCoordinates<T>>>) - Static method in class org.orekit.utils.FieldAngularCoordinates: Interpolate angular coordinates.
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, FieldPVCoordinates<T>>>) - Static method in class org.orekit.utils.FieldPVCoordinates: Interpolate position-velocity.
interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, PVCoordinates>>) - Static method in class org.orekit.utils.PVCoordinates: Interpolate position-velocity.
InterpolatingTransformProvider - Class in org.orekit.frames: Transform provider using thread-safe interpolation on transforms sample.
InterpolatingTransformProvider(TransformProvider, boolean, boolean, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider: Simple constructor.
InterpolationTableLoader - Class in org.orekit.utils: Used to read an interpolation table from a data file.
InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator: Check if an additional state is managed.
isAvailable(String) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Check if a parameter can be free.
isChildOf(Frame) - Method in class org.orekit.frames.Frame: Determine if a Frame is a child of another one.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE: Check the lines format validity.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Check is integration direction is forward in date.
isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the Increasing/decreasing status of the event.
isLof() - Method in enum org.orekit.files.ccsds.CCSDSFrame: Check if the frame is a Local Orbital frame.
isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Check if fitting uses only sample positions.
isPseudoInertial() - Method in class org.orekit.frames.Frame: Check if the frame is pseudo-inertial.
isQuasiInertial() - Method in class org.orekit.frames.Frame: Deprecated.
as of 6.0, replaced by Frame.isPseudoInertial()
isSimpleEOP() - Method in class org.orekit.files.ccsds.ODMParser: Get EOP interpolation method.
isSupported(Class<? extends DataProvider>) - Method in class org.orekit.data.DataProvidersManager: Deprecated.
as of 6.0, replaced by DataProvidersManager.isSupported(DataProvider)
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager: Check if some provider is supported.
isSupported(String) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents: J2000.0 Reference epoch: 2000-01-01.
J2DifferentialEffect - Class in org.orekit.propagation.analytical: Analytical model for J2 effect.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect: Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect: Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect: Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect: Simple constructor.
Jacobianizer - Class in org.orekit.propagation.numerical: Class helping implementation of partial derivatives in force models implementations.
Jacobianizer(ForceModel, double, Collection<ParameterConfiguration>, double) - Constructor for class org.orekit.propagation.numerical.Jacobianizer: Simple constructor.
JacobianPropagatorConverter - Class in org.orekit.propagation.conversion: Propagator converter using the real jacobian.
JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter: Simple constructor.
JacobiansMapper - Class in org.orekit.propagation.numerical: Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities: Provider of the Jacobi polynomials P_l^v,w.
JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents: Java Reference epoch: 1970-01-01.
JB2006 - Class in org.orekit.forces.drag: This is the realization of the Jacchia-Bowman 2006 atmospheric model.
JB2006(JB2006InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.JB2006: Constructor with space environment information for internal computation.
JB2006InputParameters - Interface in org.orekit.forces.drag: Interface for solar activity and magnetic activity data.
JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants: Astronomical Unit: 149597870691 m.
JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants: Earth attraction coefficient (m³/s²).
JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Earth/Moon mass ratio: 81.30059.
JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Earth + Moon) attraction coefficient (m³/s²).
JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants: Gaussian gravitational constant: 0.01720209895 √(AU³/d²).
JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Jupiter system) ttraction coefficient (m³/s²).
JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Mars system) attraction coefficient (m³/s²).
JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants: Sun/Mercury attraction coefficient (m³/s²).
JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants: Moon attraction coefficient (m³/s²).
JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Neptune system) attraction coefficient (m³/s²).
JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Pluto system) ttraction coefficient (m³/s²).
JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Saturn system) attraction coefficient (m³/s²).
JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Earth + Moon) mass ratio: 328900.56.
JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants: Sun attraction coefficient (m³/s²).
JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Jupiter system) mass ratio: 1047.3486.
JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Mars system) mass ratio: 3098708.0.
JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/Mercury mass ratio: 6023600.
JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Neptune system) mass ratio: 19412.24.
JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Pluto system) mass ratio: 1.35e8.
JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Saturn system) mass ratio: 3497.898.
JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/(Uranus system) mass ratio: 22902.98.
JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants: Sun/Venus mass ratio: 408523.71.
JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants: Sun/(Uranus system) attraction coefficient (m³/s²).
JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants: Sun/Venus attraction coefficient (m³/s²).
JPLEphemeridesLoader - Class in org.orekit.bodies: Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader: Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies: List of supported ephemerides types.
JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies: Interface for raw position-velocity retrieval.
JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants: Duration of a Julian century: 36525 Constants.JULIAN_DAY.
JULIAN_DAY - Static variable in interface org.orekit.utils.Constants: Duration of a mean solar day: 86400.0 s.
JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for julian dates: -4712-01-01.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants: Duration of a Julian year: 365.25 Constants.JULIAN_DAY.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Jupiter.

K

k - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: e_x.
KeplerianOrbit - Class in org.orekit.orbits: This class handles traditional keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit: Creates a new instance.
KeplerianOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit: Deprecated.
as of 6.0 replaced by KeplerianOrbit.KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double)
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit: Constructor from cartesian parameters.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit: Constructor from any kind of orbital parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical: Simple keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator: Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator: Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator: Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator: Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator: Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for Keplerian propagator.
KeplerianPropagatorBuilder(double, Frame) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder: Build a new instance.
Keyword - Enum in org.orekit.files.ccsds: Keywords for CCSDS orbit data messages.

L

loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader: Load celestial body.
loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader: Load celestial body.
loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries: Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader: Loads an bi-variate interpolation table from the given InputStream.
loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions: Load the Love numbers.
loadTimeSteps() - Method in interface org.orekit.time.UTCTAILoader: Load UTC-TAI offsets entries.
loadTLEData() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Load TLE data for a specified object.
loadTLEData(int) - Method in class org.orekit.propagation.analytical.tle.TLESeries: Load TLE data for a specified object.
loadTLEData(int, int, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries: Load TLE data for a specified object.
LocalOrbitalFrame - Class in org.orekit.frames: Class for frames moving with an orbiting satellite.
LocalOrbitalFrame(Frame, LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame: Build a new instance.
LofOffset - Class in org.orekit.attitudes: Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
LofOffset(Frame) - Constructor for class org.orekit.attitudes.LofOffset: Deprecated.
as of 6.0 replaced by LofOffset.LofOffset(Frame, LOFType)
LofOffset(Frame, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset: Deprecated.
as of 6.0 replaced by LofOffset.LofOffset(Frame, LOFType, RotationOrder, double, double, double)
LofOffset(Frame, LOFType) - Constructor for class org.orekit.attitudes.LofOffset: Create a LOF-aligned attitude.
LofOffset(Frame, LOFType, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset: Creates new instance.
LofOffsetPointing - Class in org.orekit.attitudes: This class provides a default attitude provider.
LofOffsetPointing(BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing: Creates new instance.
LOFType - Enum in org.orekit.frames: Enumerate for different types of Local Orbital Frames.
LoveNumbers - Class in org.orekit.utils: Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers: Simple constructor.

M

mapArrayToOrbit(double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType: Convert state array to orbital parameters.
mapArrayToState(double, double[]) - Method in class org.orekit.propagation.integration.StateMapper: Map the raw double components to a spacecraft state.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper: Map a date to a raw double time offset.
mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper: Map the raw double time offset to a date.
mapOrbitToArray(Orbit, PositionAngle, double[]) - Method in enum org.orekit.orbits.OrbitType: Convert orbit to state array.
mapStateToArray(SpacecraftState, double[]) - Method in class org.orekit.propagation.integration.StateMapper: Map a spacecraft state to raw double components.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.forces.drag: This class reads and provides solar activity data needed by atmospheric models: F107 solar flux and Kp indexes.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Simple constructor.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.forces.drag: Strength level of activity.
MASTER_MODE - Static variable in interface org.orekit.propagation.Propagator: Indicator for master mode.
MEAN_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
MEAN_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
MEAN_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic: Get mean derivative, truncated to first components.
meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic: Get mean second derivative, truncated to first components.
meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic: Get mean value, truncated to first components.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Mercury.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder: Build a new instance.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Check if missing coefficients are allowed in the input data.
ModeHandler - Interface in org.orekit.propagation.integration: Common interface for all propagator mode handlers initialization.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for modified julian dates: 1858-11-17.
MOLECULAR_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000: Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000: Identifier for molecular oxygen.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger: Monitor an event detector.
Month - Enum in org.orekit.time: Enumerate representing a calendar month.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Moon equatorial radius: 1737400 m.

N

n - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Kepler mean motion: n = sqrt(μ / a³).
NadirPointing - Class in org.orekit.attitudes: This class handles nadir pointing attitude provider.
NadirPointing(BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing: Creates new instance.
negate() - Method in class org.orekit.utils.FieldPVCoordinates: Get the opposite of the instance.
negate() - Method in class org.orekit.utils.PVCoordinates: Get the opposite of the instance.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Neptune.
NetworkCrawler - Class in org.orekit.data: Provider for data files directly fetched from network.
NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler: Build a data classpath crawler.
newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control
NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities: Implementation of the Modified Newcomb Operators.
NewtonianAttraction - Class in org.orekit.forces.gravity: Force model for Newtonian central body attraction.
NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction: Simple constructor.
NodeDetector - Class in org.orekit.propagation.events: Finder for node crossing events.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector: Build a new instance.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector: Build a new instance.
nonCentralPart(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute the non-central part of the gravity field.
NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide normalized spherical harmonics coefficients.
NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential: The normalized geopotential coefficients at a specific instance in time.
NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection: Null correction (xp = 0, yp = 0).
NumericalPropagator - Class in org.orekit.propagation.numerical: This class propagates orbits using numerical integration.
NumericalPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator: Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for numerical propagator.
NumericalPropagatorBuilder(double, Frame, FirstOrderIntegratorBuilder) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Build a new instance.

O

OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential: Supported Ocean load Deformation coefficients (Love numbers k'_i).
OceanTides - Class in org.orekit.forces.gravity: Ocean tides force model.
OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides: Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides: Simple constructor.
OceanTidesReader - Class in org.orekit.forces.gravity.potential: Reader for ocean tides coefficients.
OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader: Simple constructor.
OceanTidesWave - Class in org.orekit.forces.gravity.potential: Container for ocen tides coefficients for one tide wave.
OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave: Simple constructor.
ODMFile - Class in org.orekit.files.ccsds: The ODMFile (Orbit Data Message) class represents any of the three orbit messages used by the CCSDS, i.e.
ODMFile() - Constructor for class org.orekit.files.ccsds.ODMFile: ODMFile constructor.
ODMMetaData - Class in org.orekit.files.ccsds: This class gathers the meta-data present in the Orbital Data Message (ODM).
ODMParser - Class in org.orekit.files.ccsds: Base class for all CCSDS Orbit Data Message parsers.
ODMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String) - Constructor for class org.orekit.files.ccsds.ODMParser: Complete constructor.
OEMFile - Class in org.orekit.files.ccsds: This class stocks all the information of the OEM File parsed by OEMParser.
OEMFile() - Constructor for class org.orekit.files.ccsds.OEMFile: OEMFile constructor.
OEMFile.CovarianceMatrix - Class in org.orekit.files.ccsds: The CovarianceMatrix class represents a covariance matrix and its metadata: epoch and frame.
OEMFile.EphemeridesBlock - Class in org.orekit.files.ccsds: The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).
OEMFile.EphemeridesBlock() - Constructor for class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: EphemeridesBlock constructor.
OEMFile.EphemeridesDataLine - Class in org.orekit.files.ccsds: The EphemeridesDataLine class represents the content of an OEM ephemerides data line and consists of a cartesian orbit and an optional acceleration vector.
OEMParser - Class in org.orekit.files.ccsds: A parser for the CCSDS OEM (Orbit Ephemeris Message).
OEMParser() - Constructor for class org.orekit.files.ccsds.OEMParser: Simple constructor.
offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents: Compute the seconds offset between two instances.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Get the offset to convert locations from TAIScale to instance.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GMSTScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCBScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCGScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TDBScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UT1Scale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale: Get the offset to convert locations from instance to TAIScale.
OGMFile - Class in org.orekit.files.ccsds: This class gathers the general state data present in both OPM and OMM files.
omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final perigee argument.
omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: common parameter for perigee argument (omega) computation.
OMMFile - Class in org.orekit.files.ccsds: This class gathers the informations present in the Orbital Mean-Elements Message (OMM), and contains methods to generate a CartesianOrbit, a KeplerianOrbit, a SpacecraftState and, eventually, a TLE.
OMMFile.OMMMetaData - Class in org.orekit.files.ccsds
OMMParser - Class in org.orekit.files.ccsds: A parser for the CCSDS OMM (Orbiter Mean-Elements Message).
OMMParser() - Constructor for class org.orekit.files.ccsds.OMMParser: Simple constructor.
onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider: Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider: Get the raw spherical harmonic coefficients on a specific date.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider: Get the un-normalized spherical harmonic coefficients at a specific instance in time.
OneAxisEllipsoid - Class in org.orekit.bodies: Modeling of a one-axis ellipsoid.
OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid: Simple constructor.
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: 1 / A .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: 1 / (A * B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: 1 / (1 + B) .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: 1 / μ .
OPMFile - Class in org.orekit.files.ccsds: This class gathers the informations present in the Orbital Parameter Message (OPM), and contains methods to generate CartesianOrbit, KeplerianOrbit or SpacecraftState.
OPMFile.Maneuver - Class in org.orekit.files.ccsds: Maneuver in an OPM file.
OPMFile.Maneuver() - Constructor for class org.orekit.files.ccsds.OPMFile.Maneuver: Simple constructor.
OPMParser - Class in org.orekit.files.ccsds: A parser for the CCSDS OPM (Orbit Parameter Message).
OPMParser() - Constructor for class org.orekit.files.ccsds.OPMParser: Simple constructor.
Orbit - Class in org.orekit.orbits: This class handles orbital parameters.
Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit: Default constructor.
Orbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit: Set the orbit from Cartesian parameters.
OrbitFile - Interface in org.orekit.files.general: Interface for orbit file representations.
OrbitFile.TimeSystem - Enum in org.orekit.files.general: Time system used throughout this orbit file.
OrbitFileParser - Interface in org.orekit.files.general: Interface for orbit file parsers.
OrbitType - Enum in org.orekit.orbits: Enumerate for orbital parameters types.
OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager: Name of the property defining the root directories or zip/jar files path for default configuration.
OrekitConfiguration - Class in org.orekit.utils: Utility class for setting global configuration parameters.
OrekitException - Exception in org.orekit.errors: This class is the base class for all specific exceptions thrown by the orekit classes.
OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException: Simple constructor.
OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException: Copy constructor.
OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException: Simple constructor.
OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException: Simple constructor.
OrekitException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.OrekitException: Simple constructor.
OrekitExceptionWrapper - Exception in org.orekit.errors: This class allows to wrap OrekitException instances in RuntimeException.
OrekitExceptionWrapper(OrekitException) - Constructor for exception org.orekit.errors.OrekitExceptionWrapper: Simple constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware fixed size step handler.
OrekitMessages - Enum in org.orekit.errors: Enumeration for localized messages formats.
OrekitMessages.UTF8Control - Class in org.orekit.errors: Control class loading properties in UTF-8 encoding.
OrekitMessages.UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control
OrekitStepHandler - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step handler.
OrekitStepHandlerMultiplexer - Class in org.orekit.propagation.sampling: This class gathers several OrekitStepHandler instances into one.
OrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer: Simple constructor.
OrekitStepInterpolator - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step interpolator.
OrekitStepNormalizer - Class in org.orekit.propagation.sampling: This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer: Simple constructor.
org.orekit.attitudes - package org.orekit.attitudes: This package provides classes to represent simple attitudes.
org.orekit.bodies - package org.orekit.bodies: This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.data - package org.orekit.data: This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.errors - package org.orekit.errors: This package provides classes to generate and handle exceptions.
org.orekit.files.ccsds - package org.orekit.files.ccsds: This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
org.orekit.files.general - package org.orekit.files.general: This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.sp3 - package org.orekit.files.sp3: This package provides a parser for orbit data stored in SP3 format.
org.orekit.forces - package org.orekit.forces: This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag - package org.orekit.forces.drag
org.orekit.forces.gravity - package org.orekit.forces.gravity: This package provides all gravity-related forces.
org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential: This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers: This package provides models of simple maneuvers.
org.orekit.forces.radiation - package org.orekit.forces.radiation
org.orekit.frames - package org.orekit.frames: This package provides classes to handle frames and transforms between them.
org.orekit.models - package org.orekit.models
org.orekit.models.earth - package org.orekit.models.earth: This package provides models that simulate certain physical phenomena experienced in the atmosphere of the earth.
org.orekit.orbits - package org.orekit.orbits: This package provides classes to represent orbits.
org.orekit.propagation - package org.orekit.propagation: This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.analytical - package org.orekit.propagation.analytical
org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle: This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion - package org.orekit.propagation.conversion: This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.events - package org.orekit.propagation.events: This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers: This package provides an interface and classes dealing with events occurrence only.
org.orekit.propagation.integration - package org.orekit.propagation.integration
org.orekit.propagation.numerical - package org.orekit.propagation.numerical
org.orekit.propagation.sampling - package org.orekit.propagation.sampling: This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst: This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces
org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities
org.orekit.time - package org.orekit.time: This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils - package org.orekit.utils: This package provides useful objects.
OrphanFrame - Class in org.orekit.frames: Prototype frame that can be built from leaf to roots and later attached to a tree.
OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame: Simple constructor.
osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic: Get fitted osculating derivative.
osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic: Get fitted osculating second derivative.
OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion: This class converts osculating orbital elements into mean elements.
OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter: Constructor.
osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic: Get fitted osculating value.

P

p - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: h_y.
ParameterConfiguration - Class in org.orekit.propagation.numerical: Simple container associating a parameter name with a step to compute its jacobian and the provider that manages it.
ParameterConfiguration(String, double) - Constructor for class org.orekit.propagation.numerical.ParameterConfiguration: Parameter name and step pair constructor.
parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser: Parse a stream.
parse(String) - Method in class org.orekit.data.PolynomialParser: Parse a polynomial expression.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser: Parse a stream.
parse(String) - Method in class org.orekit.files.ccsds.ODMParser: Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.ODMParser: Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.ODMParser: Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OEMParser: Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OEMParser: Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OMMParser: Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OMMParser: Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OPMParser: Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OPMParser: Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in interface org.orekit.files.general.OrbitFileParser: Reads an orbit file from the given stream and returns a parsed OrbitFile.
parse(String) - Method in interface org.orekit.files.general.OrbitFileParser: Reads the orbit file and returns a parsed OrbitFile.
parse(String) - Method in class org.orekit.files.sp3.SP3Parser: Reads the orbit file and returns a parsed OrbitFile.
parse(InputStream) - Method in class org.orekit.files.sp3.SP3Parser: Reads an orbit file from the given stream and returns a parsed OrbitFile.
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSFrame(String) - Method in class org.orekit.files.ccsds.ODMParser: Parse a CCSDS frame.
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Parse a coefficient.
parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Parse a coefficient.
parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ODMParser: Parse a comment line.
parseDate(String, OrbitFile.TimeSystem) - Method in class org.orekit.files.ccsds.ODMParser: Parse a date.
parseDate(String) - Static method in class org.orekit.time.DateComponents: Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents: Parse a string in ISO-8601 format to build a date/time.
parseGeneralStateDataEntry(KeyValue, OGMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser: Parse a general state data key = value entry.
parseHeaderEntry(KeyValue, ODMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser: Parse an entry from the header.
parseMetaDataEntry(KeyValue, ODMMetaData, List<String>) - Method in class org.orekit.files.ccsds.ODMParser: Parse a meta-data key = value entry.
parseMonth(String) - Static method in enum org.orekit.time.Month: Parse the string to get the month.
parseTime(String) - Static method in class org.orekit.time.TimeComponents: Parse a string in ISO-8601 format to build a time.
PartialDerivativesEquations - Class in org.orekit.propagation.numerical: Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.
PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations: Simple constructor.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate: Dummy date at infinity in the past direction.
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: perigee, expressed in KM and ALTITUDE.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Pluto.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame: Compute the point observed from the station at some specified distance.
PoissonSeries<T extends RealFieldElement<T>> - Class in org.orekit.data: Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(PolynomialNutation<T>, Map<Long, SeriesTerm<T>>) - Constructor for class org.orekit.data.PoissonSeries: Build a Poisson series from an IERS table file.
PoissonSeries.CompiledSeries<S extends RealFieldElement<S>> - Interface in org.orekit.data: This interface represents a fast evaluator for Poisson series.
PoissonSeriesParser<T extends RealFieldElement<T>> - Class in org.orekit.data: Parser for Poisson series files.
PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser: Build a parser for a Poisson series from an IERS table file.
PoleCorrection - Class in org.orekit.frames: Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection: Simple constructor.
PolynomialNutation<T extends RealFieldElement<T>> - Class in org.orekit.data: Polynomial nutation function.
PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation: Build a polynomial from its coefficients.
PolynomialParser - Class in org.orekit.data: Parser for polynomials in IERS tables.
PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser: Simple constructor.
PolynomialParser.Unit - Enum in org.orekit.data: Unit for the coefficients.
PositionAngle - Enum in org.orekit.orbits: Enumerate for true, eccentric and mean position angles.
PotentialCoefficientsProvider - Interface in org.orekit.forces.gravity.potential: Deprecated.
since 6.0, replaced by UnnormalizedSphericalHarmonicsProvider
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential: This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Simple constructor.
Predefined - Enum in org.orekit.frames: Predefined frames provided by FramesFactory.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator: Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Propagate from a start date towards a target date.
propagate(AbsoluteDate, boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Propagation with or without event detection.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator: Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator: Propagate from a start date towards a target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Extrapolate an orbit up to a specific target date.
PropagationException - Exception in org.orekit.errors: This class is the base class for all specific exceptions thrown by during the propagation computation.
PropagationException(Localizable, Object...) - Constructor for exception org.orekit.errors.PropagationException: Simple constructor.
PropagationException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.PropagationException: Simple constructor.
PropagationException(OrekitException) - Constructor for exception org.orekit.errors.PropagationException: Simple constructor.
PropagationException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.PropagationException: Simple constructor.
Propagator - Interface in org.orekit.propagation: This interface provides a way to propagate an orbit at any time.
PropagatorBuilder - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction for propagators conversions.
ProviderConverter - Class in org.orekit.forces.gravity.potential: Deprecated.
this converter is temporary for 6.x series
ProviderConverter(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.potential.ProviderConverter: Deprecated.

Simple constructor.
PVCoordinates - Class in org.orekit.utils: Simple container for Position/Velocity pairs.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates: Simple constructor.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates: Builds a PVCoordinates pair.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Multiplicative constructor
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Subtractive constructor
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Linear constructor
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Linear constructor
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Linear constructor
PVCoordinatesProvider - Interface in org.orekit.utils: Interface for PV coordinates providers.

Q

q - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: h_x.

R

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to radiation pressure, with state derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Compute the acceleration due to radiation pressure, with state derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.SphericalSpacecraft: Compute the acceleration due to radiation pressure, with state derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in class org.orekit.forces.SphericalSpacecraft: Compute the acceleration due to radiation pressure, with parameters derivatives.
RadiationSensitive - Interface in org.orekit.forces.radiation: Interface for spacecraft that are sensitive to radiation pressure forces.
RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).
RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).
RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).
RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).
RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide raw spherical harmonics coefficients.
RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential: The raw spherical harmonics at a particular instant.
readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Read a gravity field coefficients provider from the first supported file.
REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive: Parameter name for reflection coefficient.
registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence: Register all wrapped switch events to the propagator.
reinitializeBegin(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.EventState: Reinitialize the beginning of the step.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Remove all perturbing force models from the global perturbation model.
removeProvider(Class<? extends DataProvider>) - Method in class org.orekit.data.DataProvidersManager: Deprecated.
as of 6.0, replaced by DataProvidersManager.removeProvider(DataProvider)
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager: Remove one provider.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Determines whether this handler needs dense output.
rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Rescale coefficients arrays.
reset(SpacecraftState) - Method in class org.orekit.propagation.events.EventState: Let the event detector reset the state if it wants.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence: Reset the active provider.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic: Reset fitting.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris: Try (and fail) to reset the initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Reset the initial state.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector: Deprecated.
as of 6.1 replaced by EventHandler.resetState(EventDetector, SpacecraftState)
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Deprecated.
as of 6.1 replaced by EventHandler.resetState(EventDetector, SpacecraftState)
resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector: Deprecated.
as of 6.1 replaced by EventHandler.resetState(EventDetector, SpacecraftState)
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent: Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler: Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing: Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnEvent: Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing: Reset the state prior to continue propagation.
revert() - Method in class org.orekit.utils.AngularCoordinates: Revert a rotation/rotation rate pair.
revert() - Method in class org.orekit.utils.FieldAngularCoordinates: Revert a FieldRotation/FieldRotation rate pair.
rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType: Get the rotation from inertial frame to local orbital frame.

S

s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: s* new value for the contant s.
SaastamoinenModel - Class in org.orekit.models.earth: The modified Saastamoinen model.
SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.SaastamoinenModel: Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SatelliteInformation - Class in org.orekit.files.general: Contains general information about a satellite as contained in an orbit file.
SatelliteInformation(String) - Constructor for class org.orekit.files.general.SatelliteInformation: Create a new SatelliteInformation object with a given satellite id.
SatelliteTimeCoordinate - Class in org.orekit.files.general: Contains the position/velocity of a satellite at an specific epoch.
SatelliteTimeCoordinate(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate: Creates a new SatelliteTimeCoordinate instance with a given epoch and coordinate.
SatelliteTimeCoordinate(AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate: Creates a new SatelliteTimeCoordinate object with a given epoch and position coordinate.
SatelliteTimeCoordinate(AbsoluteDate, PVCoordinates, double, double) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate: Creates a new SatelliteTimeCoordinate instance with a given epoch, coordinate and clock value / rate change.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Saturn.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SDP4 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SDP8 type of ephemeris.
SecularAndHarmonic - Class in org.orekit.utils: Class for fitting evolution of osculating orbital parameters.
SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic: Simple constructor.
selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Selects the extrapolator to use with the selected TLE.
selectParamAndStep(String, double) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Select the parameters to consider for Jacobian processing.
selectParameters(String...) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Select the parameters to consider for Jacobian processing.
selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType: Get next function transformer in the specified direction.
setAbsorptionCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Set the absorption coefficient.
setAbsorptionCoefficient(double) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Set the absorption coefficient.
setAbsorptionCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft: Set the absorption coefficient.
setAccuracy(int) - Method in class org.orekit.files.general.SatelliteInformation: Set the accuracy for this satellite.
setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the central body reference radius.
setAgency(String) - Method in class org.orekit.files.sp3.SP3File: Set the agency string for this SP3 file.
setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid: Set the angular convergence threshold.
setAttitudeLaw(AttitudeProvider) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Deprecated.
as of 6.0 replaced by AbstractIntegratedPropagator.setAttitudeProvider(AttitudeProvider)
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator: Set attitude provider.
setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration: Set the number of slots to use in caches.
setClockCorrection(double) - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Set the clock correction to the given value.
setClockRateChange(double) - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Set the clock rate change to the given value.
setCloseApproachThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid: Deprecated.
as of 6.1, this threshold is not used anymore
setComment(List<String>) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Set the maneuvers data comment, each string in the list corresponds to one line of comment.
setCoordinate(PVCoordinates) - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Set the coordinate for this entry.
setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3File: Set the coordinate system used for the orbit entries.
setDataUsed(String) - Method in class org.orekit.files.sp3.SP3File: Set the data used indicator for this SP3 file.
setDayFraction(double) - Method in class org.orekit.files.sp3.SP3File: Set the day fraction for this SP3 file.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Set mass change during maneuver (value is < 0).
setDragCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Set the drag coefficient.
setDragCoefficient(double) - Method in interface org.orekit.forces.drag.DragSensitive: Set the drag coefficient.
setDragCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft: Set the drag coefficient.
setDuration(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Set duration (value is 0 for impulsive maneuver).
setdV(Vector3D) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Set velocity increment.
setEphemerisMode() - Method in class org.orekit.propagation.AbstractPropagator: Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in interface org.orekit.propagation.Propagator: Set the propagator to ephemeris generation mode.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.general.SatelliteTimeCoordinate: Set the epoch for this coordinate.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3File: Set the epoch of the SP3 file.
setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3File: Set the epoch interval for this SP3 file.
setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Set the free parameters in order to build the propagator.
setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder: Set the free parameters in order to build the propagator.
setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Set the free parameters in order to build the propagator.
setFreeParameters(Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Set the free parameters in order to build the propagator.
setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Set the free parameters in order to build the propagator.
setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3File: Set the GPS week of the SP3 file.
setInitialJacobians(SpacecraftState, int, int) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Set the initial value of the Jacobian with respect to state and parameter.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the initial state with osculating orbital elements.
setInitialState(SpacecraftState, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the initial state.
setInterpolatedDate(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Set the interpolated date.
setJulianDay(int) - Method in class org.orekit.files.sp3.SP3File: Set the julian day for this SP3 file.
setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField: Set the given main field coefficients.
setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Set the initial mass.
setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.AbstractPropagator: Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator: Set the propagator to master mode with variable steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set the propagator to master mode with variable steps.
setMasterMode(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator: Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator: Set the propagator to master mode with variable steps.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Set the degree limit for the next file parsing.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the degree limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Set the order limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the order limit for the next file parsing.
setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the central body attraction coefficient.
setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set the central attraction coefficient μ.
setMuUsed() - Method in class org.orekit.files.ccsds.ODMFile: Set the gravitational coefficient created from the knowledge of the central body.
setNormalizedS(double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the normalized tesseral-sectorial coefficients matrix.
setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3File: Set the number of epochs as contained in the SP3 file.
setOrbitType(SP3File.SP3OrbitType) - Method in class org.orekit.files.sp3.SP3File: Set the SP3File.SP3OrbitType for this SP3 file.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set propagation orbit type.
setParameter(String, double) - Method in class org.orekit.forces.drag.DragForce
setParameter(String, double) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel
setParameter(String, double) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel
setParameter(String, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
setParameter(String, double) - Method in class org.orekit.forces.gravity.NewtonianAttraction
setParameter(String, double) - Method in class org.orekit.forces.gravity.OceanTides
setParameter(String, double) - Method in class org.orekit.forces.gravity.SolidTides
setParameter(String, double) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
setParameter(String, double) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
setParameter(String, double) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
setParameter(String, double) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
setParameter(String, double) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
setParameter(String, double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
setParameter(String, double) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set position angle type.
setPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper: Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set position angle type.
setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Set the local pressure at the evaluation location
setPressure(double) - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Set the local pressure at topocentric frame origin if needed.
setProvider(ForceModel) - Method in class org.orekit.propagation.numerical.ParameterConfiguration: Set the povider handling this parameter.
setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the tesseral-sectorial coefficients matrix.
setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the indicator for completed read.
setRefFrame(Frame) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Set Coordinate system for velocity increment vector, for absolute frames.
setReflectionCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Set the specular reflection coefficient.
setReflectionCoefficient(double) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Set the specular reflection coefficient.
setReflectionCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft: Set the specular reflection coefficient.
setRefLofType(LOFType) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Set coordinate system for velocity increment vector, for Local Orbital Frames.
setSatelliteId(String) - Method in class org.orekit.files.general.SatelliteInformation: Set the id of this satellite.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Override the default value of the parameter.
setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3File: Set the seconds of the GPS week for this SP3 file.
setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField: Set the given secular variation coefficients.
setSlaveMode() - Method in class org.orekit.propagation.AbstractPropagator: Set the propagator to slave mode.
setSlaveMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set the propagator to slave mode.
setSlaveMode() - Method in interface org.orekit.propagation.Propagator: Set the propagator to slave mode.
setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator: Set a start date.
setSteps(double, double) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel: Set the step for finite differences with respect to spacecraft position.
setSteps(double, double) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel: Set the step for finite differences with respect to spacecraft position.
setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Set the local temperature at the evaluation location
setTemperature(double) - Method in class org.orekit.propagation.events.ApparentElevationDetector: Deprecated.

Set the local temperature at topocentric frame origin if needed.
setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the TideSystem used in the gravity field.
setTimeout(int) - Method in class org.orekit.data.NetworkCrawler: Set the timeout for connection.
setTimeSystem(OrbitFile.TimeSystem) - Method in class org.orekit.files.sp3.SP3File: Set the time system used in this SP3 file.
setType(SP3File.SP3FileType) - Method in class org.orekit.files.sp3.SP3File: Set the file type for this SP3 file.
setUnNormalizedS(double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the un-normalized tesseral-sectorial coefficients matrix.
setUpEventDetector(AbstractIntegrator, T) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Wrap an Orekit event detector and register it to the integrator.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set up all user defined event detectors.
SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SGP type of ephemeris.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SGP4 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SGP8 type of ephemeris.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude: Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.frames.Transform: Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate: Get a time-shifted date.
shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable: Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates: Get a time-shifted state.
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential: Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader: Simple constructor.
SimpleExponentialAtmosphere - Class in org.orekit.forces.drag: Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.forces.drag.SimpleExponentialAtmosphere: Create an exponential atmosphere.
SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data: Parser for simple tables containing time stamped data.
SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser: Simple constructor.
SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data: Interface for converting a table row into time-stamped data.
sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: sinus original inclination.
SLAVE_MODE - Static variable in interface org.orekit.propagation.Propagator: Indicator for slave mode.
SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers: Analytical model for small maneuvers.
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Build a maneuver defined in user-specified frame.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for solar system barycenter.
SolarRadiationPressure - Class in org.orekit.forces.radiation: Solar radiation pressure force model.
SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure: Simple constructor with default reference values.
SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure: Complete constructor.
SolidTides - Class in org.orekit.forces.gravity: Solid tides force model.
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides: Simple constructor.
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides: Simple constructor.
SP3File - Class in org.orekit.files.sp3: Represents a parsed SP3 orbit file.
SP3File() - Constructor for class org.orekit.files.sp3.SP3File: Create a new SP3 file object.
SP3File.SP3FileType - Enum in org.orekit.files.sp3: File type indicator.
SP3File.SP3OrbitType - Enum in org.orekit.files.sp3: Orbit type indicator.
SP3Parser - Class in org.orekit.files.sp3: A parser for the SP3 orbit file format.
SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser
SpacecraftFrame - Class in org.orekit.frames: Deprecated.
as of 6.0 replaced by SpacecraftState.toTransform()
SpacecraftFrame(Propagator, String) - Constructor for class org.orekit.frames.SpacecraftFrame: Deprecated.

Simple constructor.
SpacecraftState - Class in org.orekit.propagation: This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit and attitude provider.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState: Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit and attitude provider.
SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit, attitude provider and mass.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants: Speed of light: 299792458.0 m/s.
SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide spherical harmonics coefficients.
SphericalSpacecraft - Class in org.orekit.forces: This class represents the features of a simplified spacecraft.
SphericalSpacecraft(double, double, double, double) - Constructor for class org.orekit.forces.SphericalSpacecraft: Simple constructor.
SpinStabilized - Class in org.orekit.attitudes: This class handles a spin stabilized attitude provider.
SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized: Creates a new instance.
STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: NIST standard atmospheric pressure (Pa).
STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: NIST standard atmospheric temperature (K).
startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Start parsing.
StateMapper - Class in org.orekit.propagation.integration: This class maps between raw double elements and SpacecraftState instances.
StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper: Simple constructor.
stepAccepted(SpacecraftState) - Method in class org.orekit.propagation.events.EventState: Acknowledge the fact the step has been accepted by the propagator.
stillAcceptsData() - Method in interface org.orekit.data.DataLoader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader: Check if the loader still accepts new data.
stop() - Method in class org.orekit.propagation.events.EventState: Check if the propagation should be stopped at the end of the current step.
StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing
StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Event handler which will always return stop as a state.
StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent
StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Subtract an offset from the instance.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Sun.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants: Sun radius: 695500000 m.
supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField: Indicates whether this model supports time transformation or not.
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Initialization proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Propagation proper to each propagator (SGP or SDP).

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: 3/2 * C1.
TabulatedProvider - Class in org.orekit.attitudes: This class handles an attitude provider interpolating from a predefined table.
TabulatedProvider(List<Attitude>, int, boolean) - Constructor for class org.orekit.attitudes.TabulatedProvider: Creates new instance.
TAIScale - Class in org.orekit.time: International Atomic Time.
TargetPointing - Class in org.orekit.attitudes: This class handles target pointing attitude provider.
TargetPointing(Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing: Creates a new instance from body frame and target expressed in cartesian coordinates.
TargetPointing(GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing: Creates a new instance from body shape and target expressed in geodetic coordinates.
TCBScale - Class in org.orekit.time: Barycentric Coordinate Time.
TCGScale - Class in org.orekit.time: Geocentric Coordinate Time.
TDBScale - Class in org.orekit.time: Barycentric Dynamic Time.
theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: cos io squared.
ThirdBodyAttraction - Class in org.orekit.forces.gravity: Third body attraction force model.
ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction: Simple constructor.
ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for ThreeEighthesIntegrator.
ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder: Build a new instance.
TidalCorrection - Class in org.orekit.frames: Deprecated.
as of 6.1 replaced by IERSConventions.getEOPTidalCorrection()
TidalCorrection() - Constructor for class org.orekit.frames.TidalCorrection: Deprecated.

Simple constructor.
TideSystem - Enum in org.orekit.forces.gravity.potential: Enumerate for tie systems.
TideSystemProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide tide systems.
TimeComponents - Class in org.orekit.time: Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents: Build a time from its clock elements.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents: Build a time from the second number within the day.
TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents: Build a time from the second number within the day.
TimeDerivativesEquations - Interface in org.orekit.propagation.numerical: Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeFunction<T> - Interface in org.orekit.time: This interface represents a scalar function of time.
TimeInterpolable<T extends TimeInterpolable<T>> - Interface in org.orekit.time: This interface represents objects that can be interpolated in time.
TimeScale - Interface in org.orekit.time: Interface for time scales.
TimeScalesFactory - Class in org.orekit.time: Factory for predefined time scales.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Compute the offset between two time scales at the current instant.
TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time: This interface represents objects that can be shifted in time.
TimeStamped - Interface in org.orekit.time: This interface represents objects that have a AbsoluteDate date attached to them.
TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils: Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.
TimeStampedCacheException - Exception in org.orekit.errors: This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.
TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedCacheException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils: Generator to use for creating entries in time stamped caches.
TLE - Class in org.orekit.propagation.analytical.tle: This class is a container for a single set of TLE data.
TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE: Simple constructor from unparsed two lines.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE: Simple constructor from already parsed elements.
tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: Initial state.
TLEPropagator - Class in org.orekit.propagation.analytical.tle: This class provides elements to propagate TLE's.
TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator: Protected constructor for derived classes.
TLEPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for TLEPropagator.
TLEPropagatorBuilder(int, char, int, int, String, int, int) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a new instance.
TLESeries - Class in org.orekit.propagation.analytical.tle: This class reads and handles series of TLEs for one space object.
TLESeries(String, boolean) - Constructor for class org.orekit.propagation.analytical.tle.TLESeries: Simple constructor with a TLE file.
toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates: Convert to a constant angular coordinates without derivatives.
toArray(List<List<Double>>) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Convert a list of list into an array.
toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Convert the instance to a Java Date.
toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter: Convert nutation corrections.
tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator: Estimate tolerance vectors for integrators.
tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: 2 / (n² * a) .
toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter: Convert nutation corrections.
TopocentricFrame - Class in org.orekit.frames: Topocentric frame.
TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame: Simple constructor.
toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates: Convert to a constant position-velocity without derivatives.
toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit: Convert value from instance unit to corresponding SI unit.
toString() - Method in class org.orekit.bodies.GeodeticPoint
toString() - Method in class org.orekit.frames.Frame: New definition of the java.util toString() method.
toString() - Method in class org.orekit.frames.OrphanFrame
toString() - Method in class org.orekit.models.earth.GeoMagneticElements
toString() - Method in class org.orekit.orbits.CartesianOrbit: Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.CircularOrbit: Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.EquinoctialOrbit: Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.KeplerianOrbit: Returns a string representation of this keplerian parameters object.
toString() - Method in class org.orekit.propagation.analytical.tle.TLE: Get a string representation of this TLE set.
toString() - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location in UTC time scale.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location.
toString() - Method in class org.orekit.time.DateComponents: Get a string representation (ISO-8601) of the date.
toString() - Method in class org.orekit.time.DateTimeComponents: Return a string representation of this pair.
toString() - Method in class org.orekit.time.GalileoScale
toString() - Method in class org.orekit.time.GMSTScale
toString() - Method in class org.orekit.time.GPSScale
toString() - Method in class org.orekit.time.TAIScale
toString() - Method in class org.orekit.time.TCBScale
toString() - Method in class org.orekit.time.TCGScale
toString() - Method in class org.orekit.time.TDBScale
toString() - Method in class org.orekit.time.TimeComponents: Get a string representation of the time.
toString() - Method in class org.orekit.time.TTScale
toString() - Method in class org.orekit.time.UT1Scale
toString() - Method in class org.orekit.time.UTCScale
toString() - Method in class org.orekit.utils.FieldPVCoordinates: Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache
toString() - Method in class org.orekit.utils.PVCoordinates: Return a string representation of this position/velocity pair.
toTransform() - Method in class org.orekit.propagation.SpacecraftState: Compute the transform from orbite/attitude reference frame to spacecraft frame.
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape: Transform a cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape: Transform a surface-relative point to a cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a surface-relative point to a cartesian point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a cartesian point to a surface-relative point.
Transform - Class in org.orekit.frames: Transformation class in three dimensional space.
Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a translation transform.
Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform: Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform: Build a transform by combining two existing ones.
transformFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType: Get the transform from an inertial frame defining position-velocity and the local orbital frame.
transformLine(Line) - Method in class org.orekit.frames.Transform: Transform a line.
transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField: Time transform the model coefficients from the base year of the model using secular variation coefficients.
transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField: Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.
transformPosition(Vector3D) - Method in class org.orekit.frames.Transform: Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.Transform: Transform a position vector (including translation effects).
TransformProvider - Interface in org.orekit.frames: Interface for Transform providers.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform: Transform PVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform: Transform FieldPVCoordinates including kinematic effects.
transformVector(Vector3D) - Method in class org.orekit.frames.Transform: Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.Transform: Transform a vector (ignoring translation effects).
TroposphericDelayModel - Interface in org.orekit.models.earth: Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
TRUE_ANOMALY - Static variable in class org.orekit.orbits.KeplerianOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
TRUE_LATITUDE_ARGUMENT - Static variable in class org.orekit.orbits.EquinoctialOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
TRUE_LONGITUDE_ARGUMENT - Static variable in class org.orekit.orbits.CircularOrbit: Deprecated.
as of 6.0 replaced by PositionAngle
tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: tsi from SPTRCK #3.
TTScale - Class in org.orekit.time: Terrestrial Time as defined by IAU(1991) recommendation IV.

U

UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide un-normalized spherical harmonics coefficients.
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential: Un-normalized spherical harmonics coefficients evaluated at a specific instant.
unwrap(OrekitException) - Static method in exception org.orekit.errors.PropagationException: Recover a PropagationException, possibly embedded in a OrekitException.
unwrap(ExceptionContextProvider) - Static method in exception org.orekit.errors.PropagationException: Recover a PropagationException, possibly embedded in an ExceptionContextProvider.
unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException: Recover a PropagationException, possibly embedded in a OrekitException.
unwrap(ExceptionContextProvider) - Static method in exception org.orekit.errors.TimeStampedCacheException: Recover a PropagationException, possibly embedded in an ExceptionContextProvider.
UpdatableFrame - Class in org.orekit.frames: Frame whose transform from its parent can be updated.
UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame: Build a non-inertial frame from its transform with respect to its parent.
UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame: Build a frame from its transform with respect to its parent.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator: Update state by adding all additional states.
updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Update a spacecraft mass due to maneuver.
updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame: Update the transform from parent frame implicitly according to two other frames.
UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities: Utility class to compute upper bounds for truncation algorithms.
URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Uranus.
UT1Scale - Class in org.orekit.time: Universal Time 1.
UTCScale - Class in org.orekit.time: Coordinated Universal Time.
UTCTAILoader - Interface in org.orekit.time: Interface for loading UTC-TAI offsets data files.

V

validFrom() - Method in class org.orekit.models.earth.GeoMagneticField: Returns the start of the validity period for this model.
validTo() - Method in class org.orekit.models.earth.GeoMagneticField: Returns the end of the validity period for this model.
value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries: Evaluate a set of Poisson series.
value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries: Evaluate a set of Poisson series.
value(BodiesElements) - Method in class org.orekit.data.PoissonSeries: Evaluate the value of the series.
value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries: Evaluate the value of the series.
value(double) - Method in class org.orekit.data.PolynomialNutation: Evaluate the value of the polynomial.
value(T) - Method in class org.orekit.data.PolynomialNutation: Evaluate the value of the polynomial.
value(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute the value of the gravity field.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeFunction: Compute a function of time.
valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.CCSDSFrame: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.CenterName: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.Keyword: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.general.OrbitFile.TimeSystem: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.drag.MarshallSolarActivityFutureEstimation.StrengthLevel: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.LOFType: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.Predefined: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.OrbitType: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.PositionAngle: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.EventDetector.Action: Deprecated.

Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.time.Month: Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.IERSConventions: Returns the enum constant of this type with the specified name.
values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.data.PolynomialParser.Unit: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.errors.OrekitMessages: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.CCSDSFrame: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.CenterName: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.Keyword: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.general.OrbitFile.TimeSystem: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.drag.MarshallSolarActivityFutureEstimation.StrengthLevel: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.LOFType: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.Predefined: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.OrbitType: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.PositionAngle: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.EventDetector.Action: Deprecated.

Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.FilterType: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.time.Month: Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.IERSConventions: Returns an array containing the constants of this enum type, in the order they are declared.
VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Venus.

W

w - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Equinoctial frame w vector.
WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.
WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from WGS84 model: .
WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from WGS84 model: 6378137.0 m.
WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from WGS84 model: 1.0 / 298.257223563.
WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².
withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector: Setup the minimum elevation for detection.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ODMParser: Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OEMParser: Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OMMParser: Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OPMParser: Set IERS conventions.
withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser: Set up columns for Doodson multiplers and Doodson number.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector: Setup the elevation mask for detection using the passed in mask object.
withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser: Set up first column of Delaunay multiplier.
withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser: Set up first column of planetary multiplier.
withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser: Set up column of GMST tide multiplier.
withHandler(EventHandler<T>) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Setup the event handler to call at event occurrences.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.ODMParser: Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OEMParser: Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OMMParser: Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OPMParser: Set international designator.
withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Setup the maximum checking interval.
withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Setup the maximum number of iterations in the event time search.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ODMParser: Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMParser: Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OMMParser: Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OPMParser: Set initial date.
withMu(double) - Method in class org.orekit.files.ccsds.ODMParser: Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.OEMParser: Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.OMMParser: Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.OPMParser: Set gravitational coefficient.
withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser: Set up optional column.
withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector: Setup the detector to penumbra detection.
withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser: Set up polynomial part parsing.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude: Get a similar attitude with a specific reference frame.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector: Setup the elevation detector to use an atmospheric refraction model in its calculations.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ODMParser: Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OEMParser: Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OMMParser: Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OPMParser: Set EOP interpolation method.
withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser: Set up columns of the sine and cosine coefficients.
withThreshold(double) - Method in class org.orekit.propagation.events.AbstractReconfigurableDetector: Setup the convergence threshold.
withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector: Setup the detector to full umbra detection.

X

xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: L from SPTRCK #3.
xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: common parameter for mean anomaly (M) computation.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original recovered mean motion.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: common parameter for raan (OMEGA) computation.
xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final RAAN.
xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: common parameter for raan (OMEGA) computation.

Y

YawCompensation - Class in org.orekit.attitudes: This class handles yaw compensation attitude provider.
YawCompensation(GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation: Creates a new instance.
YawSteering - Class in org.orekit.attitudes: This class handles yaw steering law.
YawSteering(GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering: Creates a new instance.

Z

ZERO - Static variable in class org.orekit.utils.PVCoordinates: Fixed position/velocity at origin (both p and v are zero vectors).
ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider: Pattern for name of zip/jar archives.
ZipJarCrawler - Class in org.orekit.data: Helper class for loading data files from a zip/jar archive.
ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler: Build a zip crawler for an archive file on filesystem.
ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler: Build a zip crawler for an archive file in classpath.
ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler: Build a zip crawler for an archive file in classpath.
ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler: Build a zip crawler for an archive file on network.

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