| getAdditionalState(String) |   | 63% | | 75% | 1 | 3 | 3 | 8 | 0 | 1 |
| getAbsPVA() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| getOrbit() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| toSpacecraftState() | | 96% | | 93% | 1 | 9 | 1 | 27 | 0 | 1 |
| getPosition(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getPVCoordinates(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| ensureCompatibleAdditionalStates(FieldSpacecraftState) | | 99% | | 84% | 4 | 14 | 2 | 33 | 0 | 1 |
| FieldSpacecraftState(Field, SpacecraftState) | | 100% | | 100% | 0 | 8 | 0 | 39 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, CalculusFieldElement, FieldDataDictionary, FieldArrayDictionary, boolean) | | 100% | | 100% | 0 | 6 | 0 | 12 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| checkDateAndFrameConsistency(FieldAttitude, FieldAbsoluteDate, Frame) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| addAdditionalData(String, Object) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| shiftAdditional(double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| shiftAdditional(CalculusFieldElement) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| withAttitude(FieldAttitude) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| toTransform() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getAdditionalData(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldDataDictionary, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| withMass(CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| withMassRate(CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| withAdditionalData(FieldDataDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| withAdditionalStatesDerivatives(FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| addAdditionalStateDerivative(String, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, FieldDataDictionary, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, CalculusFieldElement, FieldDataDictionary, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 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(FieldOrbit, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isOrbitDefined() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| checkConsistency(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getAdditionalStatesDerivatives() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalDataValues() | | 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 |