| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 22 of 758 | 97% | 3 of 40 | 92% | 4 | 31 | 5 | 92 | 2 | 11 |
| getJacobian(Orbit, PositionAngle, double[][]) | | 96% | | 86% | 2 | 12 | 3 | 31 | 0 | 1 |
| getInertialFrame() | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getInertialDV() | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | ||
| updateOrbit(Orbit) | | 100% | | 100% | 0 | 3 | 0 | 16 | 0 | 1 |
| SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) | | 100% | | 100% | 0 | 3 | 0 | 16 | 0 | 1 |
| evaluateJ0Dot() | | 100% | | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
| apply(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| apply(Orbit) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| updateMass(double) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getDate() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |