| Ephemeris(List, TimeInterpolator, List, TimeInterpolator, AttitudeProvider) |  | 100% | | 100% | 0 | 3 | 0 | 19 | 0 | 1 |
| checkStatesAndCovariancesConsistency(List, List) | | 100% | | 100% | 0 | 4 | 0 | 10 | 0 | 1 |
| basicPropagate(AbsoluteDate) | | 100% | | 100% | 0 | 3 | 0 | 17 | 0 | 1 |
| buildOrbitAndCovarianceSample() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| checkInputConsistency(List, TimeInterpolator, List, TimeInterpolator) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| isAdditionalStateManaged(String) | | 100% | | 100% | 0 | 4 | 0 | 6 | 0 | 1 |
| getManagedAdditionalStates() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getCovariance(AbsoluteDate) | | 100% |  | 66% | 2 | 4 | 0 | 6 | 0 | 1 |
| Ephemeris(List, int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| Ephemeris(List, TimeInterpolator, List, TimeInterpolator) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| Ephemeris(List, TimeInterpolator, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| Ephemeris(List, TimeInterpolator) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| resetIntermediateState(SpacecraftState, boolean) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| propagateOrbit(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMass(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCovarianceInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMinDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMaxDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStateInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| createHarvester(String, RealMatrix, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |