Class OemSatelliteEphemeris
java.lang.Object
org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
- All Implemented Interfaces:
EphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment>
public class OemSatelliteEphemeris
extends Object
implements EphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment>
OEM ephemeris blocks for a single satellite.
- Since:
- 11.0
- Author:
- Luc Maisonobe
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Constructor Summary
ConstructorsConstructorDescriptionOemSatelliteEphemeris(String id, double mu, List<OemSegment> blocks) Create a container for the set of ephemeris blocks in the file that pertain to a single satellite. -
Method Summary
Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitMethods inherited from interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
getPropagator, getPropagator
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Constructor Details
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OemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.- Parameters:
id- id of the satellite.mu- gravitational coefficient to use for building Cartesian/Keplerian orbitsblocks- containing ephemeris data for the satellite.
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Method Details
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getId
Get the satellite ID. The satellite ID is unique only within the same ephemeris file.- Specified by:
getIdin interfaceEphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment> - Returns:
- the satellite's ID, never
null.
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getMu
public double getMu()Get the standard gravitational parameter for the satellite.- Specified by:
getMuin interfaceEphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment> - Returns:
- the gravitational parameter used in
EphemerisFile.SatelliteEphemeris.getPropagator(AttitudeProvider), in m³/s².
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getSegments
Get the segments of the ephemeris.Ephemeris segments are typically used to split an ephemeris around discontinuous events, such as maneuvers.
- Specified by:
getSegmentsin interfaceEphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment> - Returns:
- the segments contained in the ephemeris file for this satellite.
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getStart
Get the start date of the ephemeris.The date returned by this method is equivalent to
getPropagator().getMinDate().- Specified by:
getStartin interfaceEphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment> - Returns:
- ephemeris start date.
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getStop
Get the end date of the ephemeris.The date returned by this method is equivalent to
getPropagator().getMaxDate().- Specified by:
getStopin interfaceEphemerisFile.SatelliteEphemeris<TimeStampedPVCoordinates,OemSegment> - Returns:
- ephemeris end date.
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