computePVCoordinates() |   | 97% |   | 85% | 2 | 8 | 1 | 90 | 0 | 1 |
TLEPropagator(TLE, AttitudeProvider, double) |  | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
initializeCommons() |  | 100% |  | 100% | 0 | 3 | 0 | 54 | 0 | 1 |
selectExtrapolator(TLE, AttitudeProvider, double, Frame) |  | 100% |  | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
TLEPropagator(TLE, AttitudeProvider, double, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
getJacobiansColumnsNames() |  | 100% |   | 87% | 1 | 5 | 0 | 8 | 0 | 1 |
resetIntermediateState(SpacecraftState, boolean) |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
resetInitialState(SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
propagateOrbit(AbsoluteDate) |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
resetTle(SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
createHarvester(String, RealMatrix, DoubleArrayDictionary) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getPVCoordinates(AbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getMass(AbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDefaultTleGenerationAlgorithm(TimeScale, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
selectExtrapolator(TLE, AttitudeProvider, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
initializeTle(TLE) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
selectExtrapolator(TLE, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
selectExtrapolator(TLE) |  | 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 |