Package org.orekit.files.ccsds

Class OEMFile.OemSatelliteEphemeris

java.lang.Object

org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris

All Implemented Interfaces:

EphemerisFile.SatelliteEphemeris

Enclosing class:

OEMFile

public static class OEMFile.OemSatelliteEphemeris
extends Object
implements EphemerisFile.SatelliteEphemeris

OEM ephemeris blocks for a single satellite.

Method Summary

Modifier and Type	Method	Description
String	getId()	Get the satellite ID.
double	getMu()	Get the standard gravitational parameter for the satellite.
List<OEMFile.EphemeridesBlock>	getSegments()	Get the segments of the ephemeris.
AbsoluteDate	getStart()	Get the start date of the ephemeris.
AbsoluteDate	getStop()	Get the end date of the ephemeris.

Methods inherited from interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

getPropagator

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Method Detail

getId

public String getId()

Description copied from interface: EphemerisFile.SatelliteEphemeris

Get the satellite ID. The satellite ID is unique only within the same ephemeris file.

Specified by:

getId in interface EphemerisFile.SatelliteEphemeris

Returns:

the satellite's ID, never null.

getMu

public double getMu()

Description copied from interface: EphemerisFile.SatelliteEphemeris

Get the standard gravitational parameter for the satellite.

Specified by:

getMu in interface EphemerisFile.SatelliteEphemeris

Returns:

the gravitational parameter use in EphemerisFile.SatelliteEphemeris.getPropagator(), in m^3 / s^2.

getSegments

public List<OEMFile.EphemeridesBlock> getSegments()

Description copied from interface: EphemerisFile.SatelliteEphemeris

Get the segments of the ephemeris.

Ephemeris segments are typically used to split an ephemeris around discontinuous events, such as maneuvers.

Specified by:

getSegments in interface EphemerisFile.SatelliteEphemeris

Returns:

the segments contained in the ephemeris file for this satellite.

getStart

public AbsoluteDate getStart()

Description copied from interface: EphemerisFile.SatelliteEphemeris

Get the start date of the ephemeris.

The date returned by this method is equivalent to getPropagator().getMinDate().

Specified by:

getStart in interface EphemerisFile.SatelliteEphemeris

Returns:

ephemeris start date.

getStop

public AbsoluteDate getStop()

Description copied from interface: EphemerisFile.SatelliteEphemeris

Get the end date of the ephemeris.

The date returned by this method is equivalent to getPropagator().getMaxDate().

Specified by:

getStop in interface EphemerisFile.SatelliteEphemeris

Returns:

ephemeris end date.