| static {...} |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| extractSigmas(double[][]) | | 100% |  | 83% | 1 | 4 | 0 | 8 | 0 | 1 |
| buildPvCovarianceMatrix(double[]) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| getCorrelationCoefficientsMatrix() | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPosition() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| theoreticalEvaluation(int, int, SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getCovarianceMatrix() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |