| realCubicRoots(double[], double[]) |   | 63% | | 50% | 5 | 7 | 16 | 39 | 0 | 1 |
| realCubicRoots(CalculusFieldElement[], CalculusFieldElement[], Field) | | 78% | | 66% | 4 | 7 | 8 | 39 | 0 | 1 |
| realQuarticRoots(CalculusFieldElement[], CalculusFieldElement[], Field) | | 82% | | 40% | 5 | 6 | 12 | 53 | 0 | 1 |
| realQuarticRoots(double[], double[]) | | 85% | | 50% | 4 | 6 | 9 | 39 | 0 | 1 |
| realQuadraticRoots(CalculusFieldElement[], CalculusFieldElement[]) | | 67% | | 37% | 4 | 5 | 8 | 19 | 0 | 1 |
| realQuadraticRoots(double[], double[]) | | 67% | | 50% | 3 | 5 | 7 | 19 | 0 | 1 |
| getLLimits(FieldSpacecraftState, FieldAuxiliaryElements) | | 98% | | 90% | 2 | 11 | 2 | 57 | 0 | 1 |
| getSpacecraft() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getEquatorialRadius() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getLLimits(SpacecraftState, AuxiliaryElements) | | 100% | | 95% | 1 | 11 | 0 | 52 | 0 | 1 |
| DSSTSolarRadiationPressure(double, double, ExtendedPositionProvider, OneAxisEllipsoid, RadiationSensitive, double) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| DSSTSolarRadiationPressure(double, double, double, double, ExtendedPositionProvider, OneAxisEllipsoid, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| DSSTSolarRadiationPressure(double, double, ExtendedPositionProvider, OneAxisEllipsoid, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| DSSTSolarRadiationPressure(ExtendedPositionProvider, OneAxisEllipsoid, RadiationSensitive, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getParametersDriversWithoutMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |