| getAdditionalState(String) |   | 72% | | 75% | 1 | 3 | 1 | 6 | 0 | 1 |
| SpacecraftState(Orbit, AbsolutePVCoordinates, Attitude, double, double, DataDictionary, DoubleArrayDictionary, boolean) | | 87% | | 80% | 2 | 6 | 0 | 12 | 0 | 1 |
| getAbsPVA() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| getOrbit() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| ensureCompatibleAdditionalStates(SpacecraftState) | | 99% | | 82% | 5 | 15 | 2 | 31 | 0 | 1 |
| shiftedBy(TimeOffset) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| checkDateAndFrameConsistency(Attitude, AbsoluteDate, Frame) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| addAdditionalData(String, Object) | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| shiftAdditional(double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| withAttitude(Attitude) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getAdditionalData(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| withMass(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| withMassRate(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| withAdditionalData(DataDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| withAdditionalStatesDerivatives(DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| SpacecraftState(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| addAdditionalStateDerivative(String, double[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, double, DataDictionary, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, double, DataDictionary, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| toTransform() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPosition(Frame) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getPVCoordinates(Frame) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| SpacecraftState(Orbit, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 3 | 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 |
| getVelocity() | | 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 |
| hasAdditionalData(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| hasAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| checkConsistency(Orbit, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isOrbitDefined() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| checkConsistency(AbsolutePVCoordinates, Attitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDefaultAttitudeProvider(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalDataValues() | | 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 |
| getMassRate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |