Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 17 of 98 | 82% | 0 of 4 | 100% | 2 | 13 | 6 | 26 | 2 | 11 |
AbstractAnalyticalPropagator.BoundedPropagatorView(AbstractAnalyticalPropagator, AbsoluteDate, AbsoluteDate) | ![]() ![]() | 87% | ![]() | 100% | 0 | 3 | 2 | 14 | 0 | 1 |
resetIntermediateState(SpacecraftState, boolean) | ![]() | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
resetInitialState(SpacecraftState) | ![]() | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
writeReplace() | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
getPVCoordinates(AbsoluteDate, Frame) | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
propagateOrbit(AbsoluteDate) | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
getMass(AbsoluteDate) | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
getInitialState() | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
getFrame() | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
getMinDate() | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
getMaxDate() | ![]() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |