| ensureCompatibleAdditionalStates(SpacecraftState) |  | 99% |   | 83% | 2 | 7 | 0 | 12 | 0 | 1 |
| interpolate(AbsoluteDate, Collection) |  | 100% |  | 100% | 0 | 6 | 0 | 23 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, double, Map) |  | 100% |  | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| checkConsistency(Orbit, Attitude) |  | 100% |  | 100% | 0 | 3 | 0 | 5 | 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 | 2 | 0 | 1 |
| SpacecraftState(Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(Orbit, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(Orbit, Map) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(Orbit, double, Map) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
| 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 |