| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 16 of 436 | 96% | 0 of 14 | 100% | 2 | 16 | 3 | 54 | 2 | 9 |
| computeDerivatives(SpacecraftState, double[]) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
| derivatives(SpacecraftState) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| combinedDerivatives(SpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 24 | 0 | 1 |
| STMEquations(CR3BPSystem) | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| getStateTransitionMatrix(SpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| setInitialPhi(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getName() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getDimension() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |