| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 6 of 264 | 98% | 1 of 16 | 94% | 1 | 18 | 2 | 60 | 0 | 10 |
| writeReplace() | | 95% | | 92% | 1 | 7 | 2 | 24 | 0 | 1 |
| KeplerianPropagator(Orbit, AttitudeProvider, double, double) | | 100% | n/a | 0 | 1 | 0 | 14 | 0 | 1 | |
| propagateOrbit(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| resetIntermediateState(SpacecraftState, boolean) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | |
| KeplerianPropagator(Orbit) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| KeplerianPropagator(Orbit, AttitudeProvider) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| KeplerianPropagator(Orbit, double) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| KeplerianPropagator(Orbit, AttitudeProvider, double) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getMass(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |