| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 0 of 75 | 100% | 0 of 2 | 100% | 0 | 8 | 0 | 17 | 0 | 7 |
| getParametersDrivers() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| ParametricAcceleration(Vector3D, boolean, AttitudeProvider, AccelerationModel) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| ParametricAcceleration(Vector3D, boolean, AccelerationModel) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| init(SpacecraftState, AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 |