| mapOrbitToArray(FieldOrbit, PositionAngle, CalculusFieldElement[], CalculusFieldElement[]) |   | 56% | | 50% | 1 | 2 | 7 | 18 | 0 | 1 |
| getDrivers(double, Orbit, PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| mapOrbitToArray(Orbit, PositionAngle, double[], double[]) | | 100% | | 100% | 0 | 2 | 0 | 18 | 0 | 1 |
| mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| mapArrayToOrbit(CalculusFieldElement[], CalculusFieldElement[], PositionAngle, FieldAbsoluteDate, CalculusFieldElement, Frame) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| convertType(Orbit) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| convertType(FieldOrbit) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| normalize(Orbit, Orbit) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| normalize(FieldOrbit, FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |