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 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, TleGenerationAlgorithm generationAlgorithm, 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 TleGenerationAlgorithmTLEPropagator.getDefaultTleGenerationAlgorithm(TLE templateTLE, TimeScale utc, Frame teme) Get the default TLE generation algorithm.static 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.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 TypeMethodDescriptionTleGenerationAlgorithm.createFromDrivers()Create orbital parameters from current drivers values.TleGenerationAlgorithm.generate(SpacecraftState state, TLE newTemplateTLE) Generate a TLE from a given spacecraft state and a template TLE.TleGenerationAlgorithm.getTemplateTLE()Get the template TLE.static TLETleGenerationUtil.newTLE(KeplerianOrbit keplerianOrbit, TLE templateTLE) 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 TypeMethodDescriptionTleGenerationAlgorithm.generate(SpacecraftState state, TLE newTemplateTLE) Generate a TLE from a given spacecraft state and a template TLE.TleGenerationAlgorithm.getJacobianWrtParameters(TLE tle) Get the Jacobian of the Cartesian coordinates with respect to the orbital elements of a TLE.static TLETleGenerationUtil.newTLE(KeplerianOrbit keplerianOrbit, TLE templateTLE) Builds a new TLE from Keplerian parameters and a template for TLE data.Constructors in org.orekit.propagation.analytical.tle.generation with parameters of type TLEModifierConstructorDescriptionFixedPointTleGenerationAlgorithm(TLE templateTLE) Default constructor.FixedPointTleGenerationAlgorithm(TLE templateTLE, double epsilon, int maxIterations, double scale) Constructor.FixedPointTleGenerationAlgorithm(TLE templateTLE, double epsilon, int maxIterations, double scale, TimeScale utc, Frame teme) Constructor.LeastSquaresTleGenerationAlgorithm(TLE templateTLE) Default constructor.LeastSquaresTleGenerationAlgorithm(TLE templateTLE, int maxIterations) Default constructor.LeastSquaresTleGenerationAlgorithm(TLE templateTLE, int maxIterations, TimeScale utc, Frame teme) Constructor.LeastSquaresTleGenerationAlgorithm(TLE templateTLE, TimeScale utc, Frame teme, LeastSquaresConverter converter) Constructor.protectedTleGenerationAlgorithm(TLE templateTLE, Frame teme, OsculatingToMeanConverter converter) Default constructor. -
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