| Package | Description |
|---|---|
| org.orekit.attitudes |
This package provides classes to represent simple attitudes.
|
| org.orekit.files.ccsds |
This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
|
| org.orekit.forces |
This package provides the interface for force models that will be used by the
NumericalPropagator, as well as
some classical spacecraft models for surface forces (spherical, box and solar array ...). |
| org.orekit.forces.drag | |
| org.orekit.forces.gravity |
This package provides all gravity-related forces.
|
| org.orekit.forces.maneuvers |
This package provides models of simple maneuvers.
|
| org.orekit.forces.radiation | |
| org.orekit.propagation |
This package provides tools to propagate orbital states with different methods.
|
| org.orekit.propagation.analytical | |
| org.orekit.propagation.analytical.tle |
This package provides classes to read and extrapolate tle's.
|
| org.orekit.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
| org.orekit.propagation.events |
This package provides interfaces and classes dealing with events occurring during propagation.
|
| org.orekit.propagation.events.handlers |
This package provides an interface and classes dealing with events occurrence only.
|
| org.orekit.propagation.integration | |
| org.orekit.propagation.numerical | |
| org.orekit.propagation.sampling |
This package provides interfaces and classes dealing with step handling during propagation.
|
| org.orekit.propagation.semianalytical.dsst |
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
|
| org.orekit.propagation.semianalytical.dsst.forces |
| Class and Description |
|---|
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| AdditionalStateProvider
This interface represents providers for additional state data beyond
SpacecraftState. |
| BoundedPropagator
This interface is intended for ephemerides valid only during a time range.
|
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| AbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
| BoundedPropagator
This interface is intended for ephemerides valid only during a time range.
|
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| AbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| AbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
| AdditionalStateProvider
This interface represents providers for additional state data beyond
SpacecraftState. |
| BoundedPropagator
This interface is intended for ephemerides valid only during a time range.
|
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| AbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| AbstractPropagator
Common handling of
Propagator methods for analytical propagators. |
| Propagator
This interface provides a way to propagate an orbit at any time.
|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
| Class and Description |
|---|
| SpacecraftState
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
|
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