| addMassDerivative(CalculusFieldElement) |   | 60% | | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
| init(FieldSpacecraftState, FieldAbsoluteDate) | | 96% | | 80% | 2 | 6 | 0 | 10 | 0 | 1 |
| computeDerivatives(FieldSpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 14 | 0 | 1 |
| addKeplerContribution(CalculusFieldElement) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| FieldNumericalPropagator.Main(FieldNumericalPropagator, FieldODEIntegrator) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| addNonKeplerianAcceleration(FieldVector3D) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| lambda$new$0(FieldODEIntegrator, FieldEventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$init$1(FieldSpacecraftState, FieldAbsoluteDate, ForceModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |