| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 58 of 145 | 60% | 5 of 12 | 58% | 9 | 16 | 13 | 33 | 6 | 10 |
| resetIntermediateState(SpacecraftState, boolean) | 0% | 0% | 2 | 2 | 4 | 4 | 1 | 1 | ||
| basicPropagate(AbsoluteDate) | 77% | 70% | 2 | 6 | 3 | 15 | 0 | 1 | ||
| resetInitialState(SpacecraftState) | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | ||
| propagateOrbit(AbsoluteDate) | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
| getMass(AbsoluteDate) | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
| getEffects() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
| getPropagator() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
| AdapterPropagator(Propagator) | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | ||
| addEffect(AdapterPropagator.DifferentialEffect) | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | ||
| getInitialState() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |