| toString() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| interpolate(FieldAbsoluteDate, Stream) |  | 83% | | 66% | 4 | 7 | 6 | 29 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, RealFieldElement) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| checkConsistency(FieldAbsolutePVCoordinates, FieldAttitude) | | 67% | | 75% | 1 | 3 | 2 | 8 | 0 | 1 |
| shiftedBy(double) | | 55% | | 50% | 1 | 2 | 1 | 3 | 0 | 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 |
| lambda$interpolate$0(FieldAbsoluteDate, List, List, List, FieldHermiteInterpolator, Map, FieldSpacecraftState) | | 93% | | 75% | 1 | 3 | 1 | 12 | 0 | 1 |
| FieldSpacecraftState(Field, SpacecraftState) | | 98% | | 95% | 1 | 12 | 1 | 57 | 0 | 1 |
| getPVCoordinates(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| ensureCompatibleAdditionalStates(FieldSpacecraftState) | | 96% | | 66% | 4 | 7 | 3 | 15 | 0 | 1 |
| toSpacecraftState() | | 100% | | 100% | 0 | 5 | 0 | 14 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, RealFieldElement, Map) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, RealFieldElement, Map) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| checkConsistency(FieldOrbit, FieldAttitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| addAdditionalState(String, RealFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| shiftedBy(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, Map) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, Map) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| toTransform() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, RealFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, RealFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 3 | 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, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, Map) | | 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 |
| getPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| FieldSpacecraftState(FieldOrbit, FieldAttitude, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isOrbitDefined() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| hasAdditionalState(String) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalStates() | | 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 |