| getInertialOrbitalProcessNoiseMatrix(SpacecraftState, SpacecraftState) |  | 100% | | 100% | 0 | 2 | 0 | 19 | 0 | 1 |
| getProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% |  | 66% | 2 | 4 | 0 | 14 | 0 | 1 |
| getPropagationProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getMeasurementsProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[], UnivariateFunction[]) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLofCartesianOrbitalParametersEvolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPropagationParametersEvolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeasurementsParametersEvolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLofType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngle() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |