| theoreticalEvaluation(int, int, SpacecraftState[]) |  | 100% | | n/a | 0 | 1 | 0 | 19 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
| AngularRaDec(Observer, Frame, AbsoluteDate, double[], MeasurementQuality, SignalTravelTimeModel, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getObservedLineOfSight(Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| AngularRaDec(Observer, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getStation() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getObserver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getReferenceFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |