| copy() |  | 0% | | 0% | 2 | 2 | 9 | 9 | 1 | 1 |
| buildPropagator(double[]) |  | 85% | | 87% | 1 | 5 | 2 | 20 | 0 | 1 |
| addForceModel(DSSTForceModel) | | 80% | | 87% | 1 | 5 | 1 | 11 | 0 | 1 |
| getPropagationType() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getStateType() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getIntegratorBuilder() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getMass() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| hasNewtonianAttraction() | | 100% | | 100% | 0 | 3 | 0 | 2 | 0 | 1 |
| buildLSModel(OrbitDeterminationPropagatorBuilder[], List, ParameterDriversList, ModelObserver) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| buildKalmanModel(List, List, ParameterDriversList, CovarianceMatrixProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| resetOrbit(Orbit, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getAllForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setMass(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |