| getOrbitalParametersDrivers(boolean) |   | 81% | | 57% | 5 | 8 | 1 | 10 | 0 | 1 |
| estimationStep(ObservedMeasurement) | | 80% | | 100% | 0 | 2 | 2 | 7 | 0 | 1 |
| getCurrentDate() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getPhysicalEstimatedState() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getPropagationParametersDrivers(boolean) | | 100% | | 90% | 1 | 6 | 0 | 10 | 0 | 1 |
| KalmanEstimator(MatrixDecomposer, List, List, ParameterDriversList) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| decorate(ObservedMeasurement) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| processMeasurements(Iterable) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| setObserver(KalmanObserver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getCurrentMeasurementNumber() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPhysicalEstimatedCovarianceMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedMeasurementsParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |