| realCubicRoots(double[], double[]) |   | 64% | | 50% | 5 | 7 | 16 | 39 | 0 | 1 |
| realQuarticRoots(double[], double[]) | | 85% | | 50% | 4 | 6 | 9 | 39 | 0 | 1 |
| realQuadraticRoots(double[], double[]) | | 68% | | 50% | 3 | 5 | 7 | 19 | 0 | 1 |
| getLLimits(SpacecraftState) | | 98% | | 85% | 3 | 11 | 1 | 51 | 0 | 1 |
| getAcceleration(SpacecraftState, Vector3D, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| getShortPeriodicVariations(AbsoluteDate, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSunSatVector(SpacecraftState, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquatorialRadius() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCr() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getArea() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |