| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 11 of 427 | 97% | 0 of 14 | 100% | 1 | 15 | 2 | 53 | 1 | 8 |
| computeDerivatives(SpacecraftState, double[]) | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | ||
| derivatives(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 |