| shiftedBy(TimeOffset) |  | 0% |  | 0% | 2 | 2 | 5 | 5 | 1 | 1 |
| toString() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| SpacecraftState(Orbit, double) |  | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| SpacecraftState(AbsolutePVCoordinates, double) |  | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| getAdditionalState(String) |   | 72% |   | 75% | 1 | 3 | 1 | 6 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, double) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 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 |
| checkDateAndFrameConsistency(Attitude, AbsoluteDate, Frame) |  | 100% |  | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| SpacecraftState(AbsolutePVCoordinates, Attitude, double, DataDictionary, DoubleArrayDictionary) |  | 100% |  | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| shiftedBy(double) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| SpacecraftState(Orbit, Attitude, double, DataDictionary, DoubleArrayDictionary) |  | 100% |  | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| addAdditionalData(String, Object) |  | 100% |  | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| shiftAdditional(double) |  | 100% |  | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| withMass(double) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| withAttitude(Attitude) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| withAdditionalData(DataDictionary) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| withAdditionalStatesDerivatives(DoubleArrayDictionary) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getAdditionalData(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(AbsolutePVCoordinates) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| addAdditionalStateDerivative(String, double[]) |  | 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 |
| 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 |
| 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(AbsolutePVCoordinates, Attitude) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |