| theoreticalEvaluation(int, int, SpacecraftState[]) |  | 100% | | 100% | 0 | 6 | 0 | 35 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | 100% | 0 | 3 | 0 | 18 | 0 | 1 |
| TDOA(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 13 | 0 | 1 |
| forwardSignalTimeOfFlight(TimeStampedFieldPVCoordinates, FieldVector3D, FieldAbsoluteDate) | | 100% |  | 75% | 1 | 3 | 0 | 10 | 0 | 1 |
| forwardSignalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) | | 100% | | 75% | 1 | 3 | 0 | 10 | 0 | 1 |
| getPrimeStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSecondStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |