| UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) |   | 60% | | 50% | 1 | 2 | 2 | 9 | 0 | 1 |
| getProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 95% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
| getInertialOrbitalProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 19 | 0 | 1 |
| getPropagationProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getLofCartesianOrbitalParametersEvolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPropagationParametersEvolution() | | 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 |