| getAdditionalState(SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getStateCovariance(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| StateCovarianceMatrixProvider(String, String, MatricesHarvester, StateCovariance) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| toRealMatrix(double[]) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| toArray(RealMatrix) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| yields(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getStateCovariance(SpacecraftState, OrbitType, PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStateCovariance(SpacecraftState, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCovarianceOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |