| initialize(AuxiliaryElements, boolean) |   | 97% | | 72% | 4 | 10 | 0 | 46 | 0 | 1 |
| getBody() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| computeUDerivatives() | | 100% | | 100% | 0 | 7 | 0 | 41 | 0 | 1 |
| getMeanElementRate(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 22 | 0 | 1 |
| initializeStep(AuxiliaryElements) | | 100% | | n/a | 0 | 1 | 0 | 32 | 0 | 1 |
| getShortPeriodicVariations(AbsoluteDate, double[]) | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
| DSSTThirdBody(CelestialBody) | | 100% | | 100% | 0 | 3 | 0 | 15 | 0 | 1 |
| computeShortPeriodicsCoefficients(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| resetShortPeriodicsCoefficients() | | 100% | | 50% | 1 | 2 | 0 | 3 | 0 | 1 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| registerAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |