| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 34 of 95 | 64% | 2 of 4 | 50% | 4 | 12 | 11 | 27 | 2 | 10 |
| AbstractAnalyticalPropagator.BoundedPropagatorView(AbstractAnalyticalPropagator, AbsoluteDate, AbsoluteDate) | | 60% | | 50% | 2 | 3 | 6 | 15 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 0% | n/a | 1 | 1 | 3 | 3 | 1 | 1 | |
| resetIntermediateState(SpacecraftState, boolean) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 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 |