| mapArrayToState(double, double[], boolean) |   | 48% | | 25% | 4 | 5 | 6 | 14 | 0 | 1 |
| computeMeanOrbit(SpacecraftState) | | 92% | | 60% | 4 | 6 | 1 | 20 | 0 | 1 |
| writeReplace() | | 86% | | 75% | 1 | 3 | 1 | 7 | 0 | 1 |
| removeForceModels() | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| computeOsculatingOrbit(SpacecraftState) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| computeShortPeriodicsCoefficients(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| mapStateToArray(SpacecraftState, double[]) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| DSSTPropagator.MeanPlusShortPeriodicMapper(AbsoluteDate, double, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| resetShortPeriodicsCoefficients() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| addForceModel(DSSTForceModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setSatelliteRevolution(int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setInitialIsOsculating(boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSatelliteRevolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| initialIsOsculating() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |