| lambda$new$1(FieldODEIntegrator, FieldEventDetector) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| lambda$new$0(FieldODEIntegrator, FieldEventDetector) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| computeDerivatives(FieldSpacecraftState) |  | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| FieldDSSTPropagator.Main(FieldDSSTPropagator, FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| lambda$new$2(FieldODEIntegrator, DSSTForceModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| init(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| elementRates(DSSTForceModel, FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$init$3(FieldSpacecraftState, FieldAbsoluteDate, DSSTForceModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |