| ensureCompatibleAdditionalStates(SpacecraftState) |  | 99% |  | 83% | 2 | 7 | 1 | 15 | 0 | 1 |
| interpolate(AbsoluteDate, Collection) | | 100% | | 100% | 0 | 6 | 0 | 28 | 0 | 1 |
| checkConsistency(Orbit, Attitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, double, Map) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
| addAdditionalState(String, double[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| toTransform() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| SpacecraftState(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(Orbit, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(Orbit, Map) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(Orbit, double, Map) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| SpacecraftState(Orbit, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| writeReplace() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasAdditionalState(String) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPVCoordinates(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getKeplerianPeriod() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getKeplerianMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLM() | | 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 |
| getPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbit() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitude() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |