| theoreticalEvaluation(int, int, SpacecraftState[]) |  | 100% |  | 91% | 1 | 7 | 0 | 46 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 27 | 0 | 1 |
| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedFieldPVCoordinates, TimeStampedFieldPVCoordinates, SpacecraftState, Map) | | 100% | | 100% | 0 | 6 | 0 | 19 | 0 | 1 |
| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedPVCoordinates, TimeStampedPVCoordinates, SpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| lambda$theoreticalEvaluation$0(EstimatedMeasurement, EstimatedMeasurement, EstimatedMeasurement, ParameterDriver) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| getEmitterStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getReceiverStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |