Package | Description |
---|---|
org.orekit.files.ccsds.ndm.odm |
This package contains class managing CCSDS Orbit Data Message.
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org.orekit.files.ccsds.ndm.odm.omm |
This package contains class managing CCSDS Orbit Mean-Elements Message.
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org.orekit.files.ccsds.ndm.odm.opm |
This package contains class managing CCSDS Orbit Parameter Message.
|
org.orekit.orbits |
This package provides classes to represent orbits.
|
org.orekit.propagation.analytical |
Top level package for analytical propagators.
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org.orekit.propagation.analytical.tle.generation |
This package provides classes related to TLE generation.
|
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
KeplerianElements.generateKeplerianOrbit(Frame frame)
Generate a keplerian orbit.
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Modifier and Type | Method and Description |
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KeplerianOrbit |
Omm.generateKeplerianOrbit()
Generate a keplerian orbit.
|
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
Opm.generateKeplerianOrbit()
Generate a keplerian orbit.
|
Modifier and Type | Method and Description |
---|---|
KeplerianOrbit |
KeplerianOrbit.removeRates()
Create a new instance such that
PositionAngleBased.hasRates() is false. |
KeplerianOrbit |
KeplerianOrbit.shiftedBy(double dt)
Get a time-shifted orbit.
|
KeplerianOrbit |
FieldKeplerianOrbit.toOrbit()
Transforms the FieldOrbit instance into an Orbit instance.
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Constructor and Description |
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FieldKeplerianOrbit(org.hipparchus.Field<T> field,
KeplerianOrbit op)
Constructor from Field and KeplerianOrbit.
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Modifier and Type | Method and Description |
---|---|
static KeplerianOrbit |
BrouwerLyddanePropagator.computeMeanOrbit(Orbit osculating,
double referenceRadius,
double mu,
double c20,
double c30,
double c40,
double c50,
double M2Value,
double epsilon,
int maxIterations)
Conversion from osculating to mean orbit.
|
static KeplerianOrbit |
BrouwerLyddanePropagator.computeMeanOrbit(Orbit osculating,
UnnormalizedSphericalHarmonicsProvider provider,
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics,
double M2Value)
Conversion from osculating to mean orbit.
|
static KeplerianOrbit |
BrouwerLyddanePropagator.computeMeanOrbit(Orbit osculating,
UnnormalizedSphericalHarmonicsProvider provider,
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics,
double M2Value,
double epsilon,
int maxIterations)
Conversion from osculating to mean orbit.
|
KeplerianOrbit |
BrouwerLyddanePropagator.propagateOrbit(AbsoluteDate date)
Extrapolate an orbit up to a specific target date.
|
Modifier and Type | Method and Description |
---|---|
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.
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