Uses of Class
org.orekit.propagation.analytical.tle.TLE
Packages that use TLE
Package
Description
This package contains class managing CCSDS Orbit Mean-Elements Message.
This package provides classes to read and extrapolate tle's.
This package provides classes related to TLE generation.
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator.This package wraps methods from various (semi)analytical models in Orekit to convert back and
forth between an averaged orbital state and an osculating one.
This package provides the ability to convert osculating orbits into mean orbits
according to different theories (Brouwer-Lyddane, Eckstein-Hechler, SGP4/SDP4,
DSST) with different conversion algorithms (fixed-point, least-squares).
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Uses of TLE in org.orekit.files.ccsds.ndm.odm.omm
Methods in org.orekit.files.ccsds.ndm.odm.omm that return TLE -
Uses of TLE in org.orekit.propagation.analytical.tle
Fields in org.orekit.propagation.analytical.tle declared as TLEMethods in org.orekit.propagation.analytical.tle that return TLEModifier and TypeMethodDescriptionTLEPropagator.getTLE()Get the underlying TLE.static TLETLE.stateToTLE(SpacecraftState state, TLE templateTLE, OsculatingToMeanConverter converter, DataContext dataContext) Convert Spacecraft State into TLE.FieldTLE.toTLE()Convert FieldTLE into TLE.Methods in org.orekit.propagation.analytical.tle with parameters of type TLEModifier and TypeMethodDescriptionstatic TLEPropagatorTLEPropagator.selectExtrapolator(TLE tle) Selects the extrapolator to use with the selected TLE.static TLEPropagatorTLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass) Selects the extrapolator to use with the selected TLE.static TLEPropagatorTLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass, Frame teme) Selects the extrapolator to use with the selected TLE.static TLEPropagatorTLEPropagator.selectExtrapolator(TLE tle, Frame teme) Selects the extrapolator to use with the selected TLE.static TLEPropagatorTLEPropagator.selectExtrapolator(TLE tle, Frame teme, AttitudeProvider attitudeProvider) Selects the extrapolator to use with the selected TLE.static TLETLE.stateToTLE(SpacecraftState state, TLE templateTLE, OsculatingToMeanConverter converter, DataContext dataContext) Convert Spacecraft State into TLE.Constructors in org.orekit.propagation.analytical.tle with parameters of type TLEModifierConstructorDescriptionDeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Constructor for a unique initial TLE.DeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Constructor for a unique initial TLE.Constructor from non-Field object.SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Constructor for a unique initial TLE.SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Constructor for a unique initial TLE.Constructor with default TEME frame.TleExtendedPositionProvider(TLE tle, Frames frames) Constructor.protectedTLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Protected constructor for derived classes.protectedTLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Protected constructor for derived classes. -
Uses of TLE in org.orekit.propagation.analytical.tle.generation
Methods in org.orekit.propagation.analytical.tle.generation that return TLEModifier and TypeMethodDescriptionFixedPointTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE) Generate a TLE from a given spacecraft state and a template TLE.LeastSquaresTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE) Generate a TLE from a given spacecraft state and a template TLE.TleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE) Generate a TLE from a given spacecraft state and a template TLE.static TLETleGenerationUtil.newTLE(KeplerianOrbit keplerianOrbit, TLE templateTLE, double bStar, TimeScale utc) Builds a new TLE from Keplerian parameters and a template for TLE data.Methods in org.orekit.propagation.analytical.tle.generation with parameters of type TLEModifier and TypeMethodDescriptionFixedPointTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE) Generate a TLE from a given spacecraft state and a template TLE.LeastSquaresTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE) Generate a TLE from a given spacecraft state and a template TLE.TleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE) Generate a TLE from a given spacecraft state and a template TLE.static TLETleGenerationUtil.newTLE(KeplerianOrbit keplerianOrbit, TLE templateTLE, double bStar, TimeScale utc) Builds a new TLE from Keplerian parameters and a template for TLE data. -
Uses of TLE in org.orekit.propagation.conversion
Methods in org.orekit.propagation.conversion that return TLEModifier and TypeMethodDescriptionTLEPropagatorBuilder.getTemplateTLE()Getter for the template TLE.Constructors in org.orekit.propagation.conversion with parameters of type TLEModifierConstructorDescriptionTLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, DataContext dataContext, TleGenerationAlgorithm generationAlgorithm) Build a new instance.TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, DataContext dataContext, TleGenerationAlgorithm generationAlgorithm, AttitudeProvider attitudeProvider) Build a new instance.TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, TleGenerationAlgorithm generationAlgorithm) Build a new instance. -
Uses of TLE in org.orekit.propagation.conversion.averaging
Methods in org.orekit.propagation.conversion.averaging with parameters of type TLE -
Uses of TLE in org.orekit.propagation.conversion.osc2mean
Constructors in org.orekit.propagation.conversion.osc2mean with parameters of type TLE