| computePVCoordinates() |   | 97% | | 85% | 2 | 8 | 1 | 90 | 0 | 1 |
| initializeCommons(double) | | 100% | | 100% | 0 | 3 | 0 | 55 | 0 | 1 |
| selectExtrapolator(TLE, AttitudeProvider, double, Frame) | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| TLEPropagator(TLE, AttitudeProvider, double, Frame) | | 100% | | n/a | 0 | 1 | 0 | 14 | 0 | 1 |
| resetBStar() | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| resetIntermediateState(SpacecraftState, boolean) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getJacobiansColumnsNames() | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| propagateOrbit(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getPVCoordinates(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| createHarvester(String, RealMatrix, DoubleArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| initializeTle(TLE) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getDefaultTleGenerationAlgorithm(TLE, TimeScale, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| TLEPropagator(TLE, AttitudeProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getMass(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| selectExtrapolator(TLE, AttitudeProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| resetTle(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| selectExtrapolator(TLE) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| selectExtrapolator(TLE, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| selectExtrapolator(TLE, Frame, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setTleGenerationAlgorithm(TleGenerationAlgorithm) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTleGenerationAlgorithm() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMU() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |