| lambda$theoreticalEvaluation$0(EstimatedMeasurement, EstimatedMeasurement, EstimatedMeasurement, ParameterDriver) |  | 0% | | 0% | 3 | 3 | 8 | 8 | 1 | 1 |
| theoreticalEvaluation(int, int, SpacecraftState[]) |  | 100% | | 100% | 0 | 4 | 0 | 38 | 0 | 1 |
| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedFieldPVCoordinates, TimeStampedFieldPVCoordinates, SpacecraftState, Map, int) | | 100% | | 100% | 0 | 7 | 0 | 26 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | 100% | 0 | 2 | 0 | 29 | 0 | 1 |
| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedPVCoordinates, TimeStampedPVCoordinates, SpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 18 | 0 | 1 |
| RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |