| Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |

# EECFI.OrbitId Member List

This is the complete list of members for EECFI.OrbitId, including all inherited members.

CfiClass() | EECFI.CfiClass |
CfiId() | EECFI.CfiId |
CfiId(CfiId cfiId) | EECFI.CfiId |
eq(final OrbitId orbitIdIn) | EECFI.OrbitId |
EECFI::CfiId.eq(CfiId cfiId) | EECFI.CfiId |
getAnx() | EECFI.OrbitId |
getOrbitInfo(long absoluteOrbit) | EECFI.OrbitId |
getOrbitNumbersFromAbs(long absOrbit) | EECFI.OrbitId |
getOrbitNumbersFromPhase(long phase) | EECFI.OrbitId |
getOrbitNumbersFromRel(long relOrbit, long cycle) | EECFI.OrbitId |
getOsf() | EECFI.OrbitId |
getOsv() | EECFI.OrbitId |
getPrecisePropagConfig() | EECFI.OrbitId |
getValTime() | EECFI.OrbitId |
init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, long driftMode, double ascMlstDrift, double inclination, long irep, long icyc, double rlong, double ascMlst) | EECFI.OrbitId |
init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, final RefOrbitInfo refOrbitInfo) | EECFI.OrbitId |
init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit) | EECFI.OrbitId |
init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId |
init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit, final PropagPreciseConf preciseConf) | EECFI.OrbitId |
init(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1, final PropagPreciseConf preciseConf) | EECFI.OrbitId |
mode() | EECFI.CfiId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, long driftMode, double ascMlstDrift, double inclination, long irep, long icyc, double rlong, double ascMlst) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, long orbit0, final RefOrbitInfo refOrbitInfo) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, double time, double[] pos, double[] vel, long absOrbit, final PropagPreciseConf preciseConf) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, final Vector< String > inputFiles, long timeInitMode, double time0, double time1, long orbit0, long orbit1, final PropagPreciseConf preciseConf) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, OsfFileVector fileData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, OrbitFileVector fileData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId |
OrbitId(final SatId satId, final ModelId modelId, final TimeCorrelation timeCor, long timeRef, long orbitFileMode, DorisFileVector fileData, long timeInitMode, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId |
OrbitId(OrbitId orbitIdIn) | EECFI.OrbitId |
osvCompute(long mode, long timeRef, double time) | EECFI.OrbitId |
osvComputeExtra(long extraChoice) | EECFI.OrbitId |
osvToTle(long timeMode, long timeRef, double time0, double time1, long orbit0, long orbit1) | EECFI.OrbitId |
resetWarning() | EECFI.CfiClass |
satId() | EECFI.OrbitId |
setAnx(final Vector< ANXExtra > anxList) | EECFI.OrbitId |
setOsf(final Vector< OsfRecords > osvRecList) | EECFI.OrbitId |
setOsv(final Vector< OsvRec > osvRecList) | EECFI.OrbitId |
setPrecisePropagConfig(final PropagPreciseConf preciseConf) | EECFI.OrbitId |
setValTime(final ValidityTime valTime) | EECFI.OrbitId |
setWarning() | EECFI.CfiClass |
status() | EECFI.CfiId |