| getOrbitalParametersDrivers(boolean) |   | 85% | | 85% | 2 | 8 | 1 | 10 | 0 | 1 |
| getBuilders() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getPropagationParametersDrivers(boolean) | | 100% | | 100% | 0 | 6 | 0 | 10 | 0 | 1 |
| AbstractKalmanEstimator(MatrixDecomposer, List) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| setObserver(KalmanObserver) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getCurrentMeasurementNumber() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCurrentDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPhysicalEstimatedState() | | 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 |
| getObserver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMatrixDecomposer() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getReferenceDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |