Uses of Class
org.orekit.propagation.analytical.tle.TLE

Packages that use TLE

Package	Description
org.orekit.files.ccsds.ndm.odm.omm	This package contains class managing CCSDS Orbit Mean-Elements Message.
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 of SpacecraftState into another propagator.
org.orekit.propagation.conversion.averaging	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.

Uses of TLE in org.orekit.files.ccsds.ndm.odm.omm

Methods in org.orekit.files.ccsds.ndm.odm.omm that return TLE

Modifier and Type	Method	Description
TLE	Omm.generateTLE()	Generate TLE from OMM file.

Uses of TLE in org.orekit.propagation.analytical.tle

Fields in org.orekit.propagation.analytical.tle declared as TLE

Modifier and Type	Field	Description
protected TLE	TLEPropagator.tle	Initial state.

Methods in org.orekit.propagation.analytical.tle that return TLE

Modifier and Type	Method	Description
TLE	TLEPropagator.getTLE()	Get the underlying TLE.
static TLE	TLE.stateToTLE(SpacecraftState state, TLE templateTLE, TleGenerationAlgorithm generationAlgorithm)	Convert Spacecraft State into TLE.
TLE	FieldTLE.toTLE()	Convert FieldTLE into TLE.

Methods in org.orekit.propagation.analytical.tle with parameters of type TLE

Modifier and Type	Method	Description
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass, Frame teme)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, Frame teme)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, Frame teme, AttitudeProvider attitudeProvider)	Selects the extrapolator to use with the selected TLE.
static TLE	TLE.stateToTLE(SpacecraftState state, TLE templateTLE, TleGenerationAlgorithm generationAlgorithm)	Convert Spacecraft State into TLE.

Constructors in org.orekit.propagation.analytical.tle with parameters of type TLE

Constructor	Description
DeepSDP4(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.
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.
TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Protected constructor for derived classes.
TLEPropagator(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 TLE

Modifier and Type	Method	Description
TLE	FixedPointTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE)	Generate a TLE from a given spacecraft state and a template TLE.
TLE	LeastSquaresTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE)	Generate a TLE from a given spacecraft state and a template TLE.
TLE	TleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE)	Generate a TLE from a given spacecraft state and a template TLE.
static TLE	TleGenerationUtil.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 TLE

Modifier and Type	Method	Description
TLE	FixedPointTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE)	Generate a TLE from a given spacecraft state and a template TLE.
TLE	LeastSquaresTleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE)	Generate a TLE from a given spacecraft state and a template TLE.
TLE	TleGenerationAlgorithm.generate(SpacecraftState state, TLE templateTLE)	Generate a TLE from a given spacecraft state and a template TLE.
static TLE	TleGenerationUtil.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 TLE

Modifier and Type	Method	Description
TLE	TLEPropagatorBuilder.getTemplateTLE()	Getter for the template TLE.

Constructors in org.orekit.propagation.conversion with parameters of type TLE

Constructor	Description
TLEPropagatorBuilder(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

Modifier and Type	Method	Description
static SGP4OrbitalState	SGP4OrbitalState.of(TLE tle, Frame teme)	Static constructor.