| basicPropagate(AbsoluteDate) |   | 79% | | n/a | 0 | 1 | 2 | 6 | 0 | 1 |
| propagate(AbsoluteDate, AbsoluteDate) | | 96% | | 100% | 0 | 5 | 2 | 28 | 0 | 1 |
| getPvProvider() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getJacobiansColumnsNames() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| acceptStep(OrekitStepInterpolator, AbsoluteDate) | | 100% | | 97% | 1 | 23 | 0 | 64 | 0 | 1 |
| AbstractAnalyticalPropagator(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| getEventDetectors() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| checkStartDateIsNotInfinity(AbsoluteDate) | | 100% | | 75% | 1 | 3 | 0 | 3 | 0 | 1 |
| addEventDetector(EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| lambda$getEphemerisGenerator$0() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$acceptStep$1(SpacecraftState, AbsoluteDate, EventState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| clearEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEphemerisGenerator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |