| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedFieldPVCoordinates, TimeStampedFieldPVCoordinates, SpacecraftState, Map) |  | 98% |  | 80% | 2 | 6 | 0 | 19 | 0 | 1 |
| oneWayTheoreticalEvaluation(int, int, boolean, TimeStampedPVCoordinates, TimeStampedPVCoordinates, SpacecraftState) | | 96% | | 50% | 2 | 3 | 0 | 9 | 0 | 1 |
| theoreticalEvaluation(int, int, SpacecraftState[]) | | 100% | | 90% | 2 | 11 | 0 | 51 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | 87% | 1 | 5 | 0 | 28 | 0 | 1 |
| FDOA(GroundStation, GroundStation, double, AbsoluteDate, double, double, double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 14 | 0 | 1 |
| lambda$theoreticalEvaluation$0(EstimatedMeasurement, EstimatedMeasurement, double, EstimatedMeasurement, ParameterDriver) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| linkDelay(FieldVector3D, FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| linkDelay(Vector3D, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPrimeStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSecondStation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |