| findRoot(OrekitStepInterpolator, AbsoluteDate, double, AbsoluteDate, double) |   | 89% | | 84% | 11 | 36 | 3 | 77 | 0 | 1 |
| check(boolean) | | 37% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| doEvent(SpacecraftState) | | 98% | | 80% | 2 | 6 | 0 | 14 | 0 | 1 |
| tryAdvance(SpacecraftState, OrekitStepInterpolator) | | 98% | | 93% | 1 | 9 | 0 | 15 | 0 | 1 |
| minTime(AbsoluteDate, AbsoluteDate) | | 93% | | 75% | 1 | 3 | 0 | 1 | 0 | 1 |
| evaluateStep(OrekitStepInterpolator) | | 100% | | 92% | 1 | 8 | 0 | 21 | 0 | 1 |
| reinitializeBegin(OrekitStepInterpolator) | | 100% | | 100% | 0 | 5 | 0 | 15 | 0 | 1 |
| EventState(EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 15 | 0 | 1 |
| shiftedBy(AbsoluteDate, double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| strictlyAfter(AbsoluteDate, AbsoluteDate) | | 100% | | 90% | 1 | 6 | 0 | 3 | 0 | 1 |
| g(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| nextAfter(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| lambda$findRoot$0(OrekitStepInterpolator, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEventDetector() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEventDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |