| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 14 of 326 | 95% | 3 of 28 | 89% | 3 | 22 | 1 | 52 | 0 | 8 |
| addMassDerivative(double) | | 52% | | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 95% | | 80% | 2 | 6 | 0 | 9 | 0 | 1 |
| computeDerivatives(SpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
| addKeplerContribution(double) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| NumericalPropagator.Main(NumericalPropagator, ODEIntegrator) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| addNonKeplerianAcceleration(Vector3D) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| lambda$new$0(ODEIntegrator, EventDetector) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| lambda$init$1(SpacecraftState, AbsoluteDate, ForceModel) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |