| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 46 of 210 | 78% | 3 of 10 | 70% | 8 | 18 | 9 | 37 | 5 | 13 |
| writeReplace() | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| resetInitialState(SpacecraftState) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| isAdditionalStateManaged(String) | | 81% | | 50% | 3 | 4 | 2 | 6 | 0 | 1 |
| basicPropagate(AbsoluteDate) | | 68% | n/a | 0 | 1 | 2 | 4 | 0 | 1 | |
| getPVCoordinates(AbsoluteDate, Frame) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| propagateOrbit(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getMass(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| Ephemeris(List, int) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| getManagedAdditionalStates() | | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | |
| getInitialState() | | 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 | |
| getFrame() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |