| Package | Description |
|---|---|
| org.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.tle |
This package provides classes to read and extrapolate tle's.
|
| org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
|
| Modifier and Type | Class | Description |
|---|---|---|
class |
AdapterPropagator |
Orbit propagator that adapts an underlying propagator, adding
differential effects. |
class |
AggregateBoundedPropagator |
A
BoundedPropagator that covers a larger time span from several constituent
propagators that cover shorter time spans. |
class |
EcksteinHechlerPropagator |
This class propagates a
SpacecraftState
using the analytical Eckstein-Hechler model. |
class |
Ephemeris |
This class is designed to accept and handle tabulated orbital entries.
|
class |
KeplerianPropagator |
Simple Keplerian orbit propagator.
|
| Modifier and Type | Class | Description |
|---|---|---|
class |
GPSPropagator |
This class aims at propagating a GPS orbit from
GPSOrbitalElements. |
| Modifier and Type | Class | Description |
|---|---|---|
class |
DeepSDP4 |
This class contains the methods that compute deep space perturbation terms.
|
class |
SGP4 |
This class contains methods to compute propagated coordinates with the SGP4 model.
|
class |
TLEPropagator |
This class provides elements to propagate TLE's.
|
| Modifier and Type | Class | Description |
|---|---|---|
class |
IntegratedEphemeris |
This class stores sequentially generated orbital parameters for
later retrieval.
|
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