| resetInitialState(FieldSpacecraftState) |   | 73% | | 50% | 1 | 2 | 1 | 5 | 0 | 1 |
| removeForceModels() | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getNewtonianAttractionForceModel() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getOrbitType() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| tolerances(RealFieldElement, FieldOrbit, OrbitType) | | 100% | | 100% | 0 | 4 | 0 | 30 | 0 | 1 |
| FieldNumericalPropagator(Field, FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| createMapper(FieldAbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setMu(double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| addForceModel(ForceModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPVCoordinates(FieldAbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMainStateEquations(FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setOrbitType(OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPositionAngleType(PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |