| checkConsistency(AbsolutePVCoordinates, Attitude) |   | 29% | | 50% | 2 | 3 | 5 | 8 | 0 | 1 |
| toString() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| SpacecraftState(AbsolutePVCoordinates, double) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| getAbsPVA() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| getOrbit() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| getPosition(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getPVCoordinates(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| ensureCompatibleAdditionalStates(SpacecraftState) | | 98% | | 83% | 4 | 13 | 2 | 31 | 0 | 1 |
| getA() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getEquinoctialEx() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getE() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| checkConsistency(Orbit, Attitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| addAdditionalState(String, double[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| addAdditionalStateDerivative(String, double[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| shiftAdditional(double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| toTransform() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 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(AbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(Orbit, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(Orbit, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| writeReplace() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getDate() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getPosition() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| toStaticTransform() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| hasAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getKeplerianPeriod() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getKeplerianMeanMotion() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getLv() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getLE() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getLM() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getI() | | 100% | | 100% | 0 | 2 | 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, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isOrbitDefined() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getDefaultAttitudeProvider(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalStatesValues() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalStatesDerivatives() | | 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 |