| getParameterDerivatives(ParameterDriver) |   | 36% | | 50% | 1 | 2 | 2 | 4 | 0 | 1 |
| setParameterDerivatives(ParameterDriver, AbsoluteDate, double[]) | | 87% | | 75% | 2 | 5 | 1 | 13 | 0 | 1 |
| getParameterDerivatives(ParameterDriver, AbsoluteDate) | | 100% | | 100% | 0 | 5 | 0 | 11 | 0 | 1 |
| setStateDerivatives(int, double[][]) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getStateDerivatives(int) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| EstimatedMeasurement(EstimatedMeasurementBase) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| EstimatedMeasurement(ObservedMeasurement, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getStateSize() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setParameterDerivatives(ParameterDriver, TimeSpanMap) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDerivativesDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |