| getPrimaryStation() |  | 0% | | 0% | 2 | 2 | 3 | 3 | 1 | 1 |
| getSecondaryStation() | | 0% | | 0% | 2 | 2 | 3 | 3 | 1 | 1 |
| theoreticalEvaluation(int, int, SpacecraftState[]) |  | 100% | | 92% | 1 | 8 | 0 | 69 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 50 | 0 | 1 |
| TurnAroundRange(Observer, Observer, AbsoluteDate, double, double, double, SignalTravelTimeModel, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| TurnAroundRange(Observer, Observer, AbsoluteDate, double, double, double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPrimaryObserver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSecondaryObserver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |