| lambda$setUpInternalDetectors$2(FieldEventDetector) |  | 0% | | 0% | 2 | 2 | 1 | 1 | 1 | 1 |
| NumericalPropagator.Main(NumericalPropagator, ODEIntegrator, OrbitType, PositionAngleType, List) |  | 95% | | 80% | 2 | 6 | 0 | 10 | 0 | 1 |
| setUpInternalDetectors(ODEIntegrator) | | 100% | | 100% | 0 | 3 | 0 | 15 | 0 | 1 |
| setUpInternalEventDetector(ODEIntegrator, EventDetector, NumericalTimeDerivativesEquations, List) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| computeDerivatives(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| lambda$setUpInternalDetectors$1(FieldEventDetector) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| lambda$setUpInternalDetectors$4(ODEIntegrator, NumericalTimeDerivativesEquations, List, EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$setUpInternalDetectors$3(ODEIntegrator, NumericalTimeDerivativesEquations, List, EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$init$5(SpacecraftState, AbsoluteDate, ForceModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$setUpInternalDetectors$0(GradientField, ForceModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |