generateKeplerianOrbit() | | 74% | | 50% | 1 | 2 | 1 | 6 | 0 | 1 |
generateTLE() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
OMMFile() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
generateSpacecraftState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setTLERelatedParametersComment(List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
generateCartesianOrbit() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setbStar(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setMeanMotionDot(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setMeanMotionDotDot(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getCoordinateSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setMeanMotion(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEphemerisType(int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setClassificationType(char) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setNoradID(Integer) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setElementSetNo(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setRevAtEpoch(int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getBStar() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotionDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotionDotDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTLERelatedParametersComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTimeSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMetaData() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEphemerisType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getClassificationType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNoradID() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getElementSetNumber() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRevAtEpoch() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |