| getSpacecraft() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D) |  | 100% | | 100% | 0 | 2 | 0 | 28 | 0 | 1 |
| isStateDerivative(FieldSpacecraftState) | | 100% | | 70% | 6 | 11 | 0 | 14 | 0 | 1 |
| acceleration(FieldSpacecraftState, RealFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| isVariable(DerivativeStructure, int) | | 100% | | 100% | 0 | 4 | 0 | 5 | 0 | 1 |
| DragForce(Atmosphere, DragSensitive) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAtmosphere() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFieldEventsDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |