| validate(double) |  | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| generateKeplerianOrbit(Frame, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| KeplerianElements() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| setA(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setMu(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setEpoch(AbsoluteDate) | | 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 |
| setMeanMotion(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEpoch() | | 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 |