Uses of Package
org.orekit.propagation

Packages that use org.orekit.propagation Package Description org.orekit.attitudes This package provides classes to represent simple attitudes.org.orekit.control.indirect.adjoint This package provides routines to model the adjoint dynamics as in the Pontryagin Maximum Principle, as used in indirect control.org.orekit.control.indirect.shooting This package provides routines to solve indirect optimal control within the frame of orbital mechanics, using shooting methods.org.orekit.estimation.leastsquares The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.org.orekit.estimation.measurements The measurements package defines everything that is related to orbit determination measurements.org.orekit.estimation.measurements.filtering This package provides measurement preprocessing filters.org.orekit.estimation.measurements.generation This package provides Orbit Determination measurements generation.org.orekit.estimation.measurements.gnss This package provides methods to handle GNSS measurements.org.orekit.estimation.measurements.modifiers This package provides measurement modifier.org.orekit.estimation.sequential The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.org.orekit.files.ccsds.ndm.adm.aem This package contains class managing CCSDS Attitude Ephemeris Message.org.orekit.files.ccsds.ndm.odm.ocm This package contains class managing CCSDS Orbit Comprehensive Message.org.orekit.files.ccsds.ndm.odm.oem This package contains class managing CCSDS Orbit Ephemeris Message.org.orekit.files.ccsds.ndm.odm.omm This package contains class managing CCSDS Orbit MeanElements Message.org.orekit.files.ccsds.ndm.odm.opm This package contains class managing CCSDS Orbit Parameter Message.org.orekit.files.general This package provides interfaces for orbit file representations and corresponding parsers.org.orekit.files.ilrs This package provides parsers for laser ranging data stored in CDR and CPF formats.org.orekit.files.sp3 This package provides a parser for orbit data stored in SP3 format.org.orekit.forces This package provides the interface for force models that will be used by theNumericalPropagator
, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).org.orekit.forces.drag This package provides all dragrelated forces.org.orekit.forces.empirical This package provides empirical forces.org.orekit.forces.gravity This package provides all gravityrelated forces.org.orekit.forces.inertia This package provides inertial force model.org.orekit.forces.maneuvers This package provides models of simple maneuvers.org.orekit.forces.maneuvers.jacobians Generators for columns of Jacobian matrices related to maneuver parameters.org.orekit.forces.maneuvers.propulsion This package provides propulsion models intended to be used with classManeuver
.org.orekit.forces.maneuvers.trigger This package provides maneuver triggers' models intended to be used with classManeuver
.org.orekit.forces.radiation This package provides all radiation pressure related forces.org.orekit.gnss This package provides classes related to GNSS applications.org.orekit.models.earth.ionosphere This package provides models that simulate the impact of the ionosphere.org.orekit.orbits This package provides classes to represent orbits.org.orekit.propagation Propagationorg.orekit.propagation.analytical Top level package for analytical propagators.org.orekit.propagation.analytical.gnss This package provides classes to propagate GNSS orbits.org.orekit.propagation.analytical.intelsat This package provides classes to propagate Intelsat's 11 elements.org.orekit.propagation.analytical.tle This package provides classes to read and extrapolate tle's.org.orekit.propagation.analytical.tle.generation This package provides classes related to TLE generation.org.orekit.propagation.conversion This package provides tools to convert a given propagator or a set ofSpacecraftState
into another propagator.org.orekit.propagation.events This package provides interfaces and classes dealing with events occurring during propagation.org.orekit.propagation.events.handlers This package provides an interface and classes dealing with events occurrence only.org.orekit.propagation.integration Utilities for integrationbased propagators (both numerical and semianalytical).org.orekit.propagation.numerical Top level package for numerical propagators.org.orekit.propagation.numerical.cr3bp Top level package for CR3BP Models used with a numerical propagator.org.orekit.propagation.sampling This package provides interfaces and classes dealing with step handling during propagation.org.orekit.propagation.semianalytical.dsst This package provides an implementation of the Draper Semianalytical Satellite Theory (DSST).org.orekit.propagation.semianalytical.dsst.forces This package provides force models for Draper Semianalytical Satellite Theory (DSST).org.orekit.ssa.collision.shorttermencounter.probability.twod Package specific to calculus assuming a 2D shortterm encounter model.org.orekit.utils This package provides useful objects. 
Classes in org.orekit.propagation used by org.orekit.attitudes Class Description FieldPropagator This interface provides a way to propagate an orbit at any time.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.control.indirect.adjoint Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.control.indirect.shooting Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.estimation.leastsquares Class Description MatricesHarvester Interface for extracting State Transition Matrices and Jacobians matrices fromspacecraft state
.PropagationType Enumerate to define the propagation type used by the propagator.Propagator This interface provides a way to propagate an orbit at any time. 
Classes in org.orekit.propagation used by org.orekit.estimation.measurements Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.estimation.measurements.filtering Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.estimation.measurements.generation Class Description Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.estimation.measurements.gnss Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.estimation.measurements.modifiers Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.estimation.sequential Class Description Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.ccsds.ndm.adm.aem Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.ccsds.ndm.odm.ocm Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.ccsds.ndm.odm.oem Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.ccsds.ndm.odm.omm Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.ccsds.ndm.odm.opm Class Description SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.general Class Description AbstractPropagator Common handling ofPropagator
methods for analytical propagators.BoundedPropagator This interface is intended for ephemerides valid only during a time range.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.ilrs Class Description BoundedPropagator This interface is intended for ephemerides valid only during a time range.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.files.sp3 Class Description BoundedPropagator This interface is intended for ephemerides valid only during a time range. 
Classes in org.orekit.propagation used by org.orekit.forces Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.drag Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.empirical Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.gravity Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.inertia Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.maneuvers Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.maneuvers.jacobians Class Description AdditionalStateProvider This interface allows to modifySpacecraftState
and set up additional state data.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.maneuvers.propulsion Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.maneuvers.trigger Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.forces.radiation Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.gnss Class Description Propagator This interface provides a way to propagate an orbit at any time. 
Classes in org.orekit.propagation used by org.orekit.models.earth.ionosphere Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.orbits Class Description Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation Class Description AbstractMatricesHarvester Base harvester between twodimensional Jacobian matrices and onedimensionaladditional state arrays
.AbstractStateCovarianceInterpolator Abstract class for orbit and state covariance interpolator.AdditionalStateProvider This interface allows to modifySpacecraftState
and set up additional state data.BoundedPropagator This interface is intended for ephemerides valid only during a time range.EphemerisGenerator Generator for ephemerides.FieldAdditionalStateProvider This interface allows to modifyFieldSpacecraftState
and set up additional state data.FieldBoundedPropagator This interface is intended for ephemerides valid only during a time range.FieldEphemerisGenerator Generator for ephemerides.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.FieldStateCovariance This class is the representation of a covariance matrix at a given date.MatricesHarvester Interface for extracting State Transition Matrices and Jacobians matrices fromspacecraft state
.PropagationType Enumerate to define the propagation type used by the propagator.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.StateCovariance This class is the representation of a covariance matrix at a given date. 
Classes in org.orekit.propagation used by org.orekit.propagation.analytical Class Description AbstractMatricesHarvester Base harvester between twodimensional Jacobian matrices and onedimensionaladditional state arrays
.AbstractPropagator Common handling ofPropagator
methods for analytical propagators.AdditionalStateProvider This interface allows to modifySpacecraftState
and set up additional state data.BoundedPropagator This interface is intended for ephemerides valid only during a time range.EphemerisGenerator Generator for ephemerides.FieldAbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldEphemerisGenerator Generator for ephemerides.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.MatricesHarvester Interface for extracting State Transition Matrices and Jacobians matrices fromspacecraft state
.PropagationType Enumerate to define the propagation type used by the propagator.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.StateCovariance This class is the representation of a covariance matrix at a given date. 
Classes in org.orekit.propagation used by org.orekit.propagation.analytical.gnss Class Description AbstractPropagator Common handling ofPropagator
methods for analytical propagators.AdditionalStateProvider This interface allows to modifySpacecraftState
and set up additional state data.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.analytical.intelsat Class Description AbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldAbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.analytical.tle Class Description AbstractMatricesHarvester Base harvester between twodimensional Jacobian matrices and onedimensionaladditional state arrays
.AbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldAbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.analytical.tle.generation Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.conversion Class Description PropagationType Enumerate to define the propagation type used by the propagator.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.events Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.events.handlers Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.integration Class Description AbstractPropagator Common handling ofPropagator
methods for analytical propagators.AdditionalStateProvider This interface allows to modifySpacecraftState
and set up additional state data.BoundedPropagator This interface is intended for ephemerides valid only during a time range.EphemerisGenerator Generator for ephemerides.FieldAbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldAdditionalStateProvider This interface allows to modifyFieldSpacecraftState
and set up additional state data.FieldBoundedPropagator This interface is intended for ephemerides valid only during a time range.FieldEphemerisGenerator Generator for ephemerides.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.PropagationType Enumerate to define the propagation type used by the propagator.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.numerical Class Description AbstractMatricesHarvester Base harvester between twodimensional Jacobian matrices and onedimensionaladditional state arrays
.AbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldAbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.numerical.cr3bp Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.sampling Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.semianalytical.dsst Class Description AbstractMatricesHarvester Base harvester between twodimensional Jacobian matrices and onedimensionaladditional state arrays
.AbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldAbstractPropagator Common handling ofPropagator
methods for analytical propagators.FieldPropagator This interface provides a way to propagate an orbit at any time.FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.MatricesHarvester Interface for extracting State Transition Matrices and Jacobians matrices fromspacecraft state
.PropagationType Enumerate to define the propagation type used by the propagator.Propagator This interface provides a way to propagate an orbit at any time.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.propagation.semianalytical.dsst.forces Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.PropagationType Enumerate to define the propagation type used by the propagator.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation. 
Classes in org.orekit.propagation used by org.orekit.ssa.collision.shorttermencounter.probability.twod Class Description FieldStateCovariance This class is the representation of a covariance matrix at a given date.StateCovariance This class is the representation of a covariance matrix at a given date. 
Classes in org.orekit.propagation used by org.orekit.utils Class Description FieldSpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.FieldStateCovariance This class is the representation of a covariance matrix at a given date.SpacecraftState This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.StateCovariance This class is the representation of a covariance matrix at a given date.