| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 0 of 87 | 100% | 0 of 6 | 100% | 0 | 10 | 0 | 21 | 0 | 7 |
| TrajectoryState(OrbitElementsType, AbsoluteDate, String[], int, List) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| TrajectoryState(OrbitElementsType, AbsoluteDate, double[]) | | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | |
| getAvailableDerivatives() | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
| toCartesian(OneAxisEllipsoid, double) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getElements() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getDate() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getType() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |