| computeUpdateMatrix(SpacecraftState) |  | 100% | | 100% | 0 | 4 | 0 | 17 | 0 | 1 |
| updateState(SpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
| buildCartesianState(SpacecraftState, TimeStampedPVCoordinates) | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate, EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| evaluateG(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| findSwitchDetector(EventDetector, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| findSwitchDetector(double, FieldSpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| shift(SpacecraftState, double) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| eventOccurred(SpacecraftState, EventDetector, boolean) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| SwitchEventHandler(EventHandler, NumericalPropagationHarvester, NumericalTimeDerivativesEquations, AttitudeProvider, List) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| resetState(EventDetector, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| lambda$findSwitchDetector$1(FieldSpacecraftState, FieldEventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$init$0(FieldSpacecraftState, FieldAbsoluteDate, FieldEventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |