| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 21 of 109 | 80% | 0 of 0 | n/a | 1 | 10 | 3 | 20 | 1 | 10 |
| acceleration(SpacecraftState, double[]) | | 0% | n/a | 1 | 1 | 3 | 3 | 1 | 1 | |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| NewtonianAttraction(double) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| getMu(Field, FieldAbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| addContribution(SpacecraftState, TimeDerivativesEquations) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getMu(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| static {...} | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getParametersDrivers() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| dependsOnPositionOnly() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |