| FieldKeplerianPropagator(FieldOrbit, AttitudeProvider, RealFieldElement) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| resetInitialState(FieldSpacecraftState) |  | 91% | | 50% | 1 | 2 | 0 | 8 | 0 | 1 |
| FieldKeplerianPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| fixState(FieldOrbit, FieldAttitude, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| propagateOrbit(FieldAbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| FieldKeplerianPropagator(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldKeplerianPropagator(FieldOrbit, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldKeplerianPropagator(FieldOrbit, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |