validate(double) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
KeplerianElements() | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
generateKeplerianOrbit(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setEpoch(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setA(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setE(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setI(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setRaan(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setPa(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setAnomaly(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setAnomalyType(PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setMu(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
setMeanMotion(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEpoch() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRaan() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPa() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAnomaly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAnomalyType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |