| oneWayTheoreticalEvaluation(int, int, FieldPVCoordinatesProvider, SpacecraftState, Map, int) |  | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
| twoWayTheoreticalEvaluation(int, int, FieldPVCoordinatesProvider, SpacecraftState, Map, int) | | 100% | | n/a | 0 | 1 | 0 | 20 | 0 | 1 |
| oneWayTheoreticalEvaluationWithoutDerivatives(int, int, AbsoluteDate, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 15 | 0 | 1 |
| twoWayTheoreticalEvaluationWithoutDerivatives(int, int, AbsoluteDate, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| RangeRate(Observer, AbsoluteDate, double, double, double, boolean, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| RangeRate(Observer, AbsoluteDate, double, MeasurementQuality, boolean, SignalTravelTimeModel, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |