| toString() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getEquinoctialEx() |  | 47% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 47% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getE() | | 47% | | 50% | 1 | 2 | 0 | 1 | 0 | 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(FieldSpacecraftState) | | 98% | | 83% | 4 | 13 | 2 | 31 | 0 | 1 |
| FieldSpacecraftState(Field, SpacecraftState) | | 100% | | 100% | 0 | 10 | 0 | 44 | 0 | 1 |
| toSpacecraftState() | | 100% | | 100% | 0 | 8 | 0 | 23 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldArrayDictionary, FieldArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| checkConsistency(FieldOrbit, FieldAttitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, FieldArrayDictionary, FieldArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| checkConsistency(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| addAdditionalState(String, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| addAdditionalStateDerivative(String, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| shiftAdditional(double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| shiftAdditional(CalculusFieldElement) | | 100% | | 100% | 0 | 4 | 0 | 9 | 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 |
| FieldSpacecraftState(FieldOrbit, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldArrayDictionary) | | 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 |
| 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 |
| getA() | | 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 |
| FieldSpacecraftState(FieldOrbit, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, 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 |
| 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 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isOrbitDefined() | | 100% | | 100% | 0 | 2 | 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 |