| theoreticalEvaluation(int, int, SpacecraftState[]) |  | 100% | | 100% | 0 | 6 | 0 | 53 | 0 | 1 |
| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedFieldPVCoordinates, TimeStampedFieldPVCoordinates, SpacecraftState, Map) | | 100% | | 100% | 0 | 5 | 0 | 18 | 0 | 1 |
| RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, int) | | 100% | | n/a | 0 | 1 | 0 | 13 | 0 | 1 |
| lambda$theoreticalEvaluation$0(EstimatedMeasurement, EstimatedMeasurement, EstimatedMeasurement, ParameterDriver) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isTwoWay() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |