| mapOrbitToArray(FieldOrbit, PositionAngle, RealFieldElement[], RealFieldElement[]) |   | 45% | | 25% | 2 | 3 | 8 | 17 | 0 | 1 |
| getDrivers(double, Orbit, PositionAngle) | | 98% | | 75% | 1 | 3 | 0 | 12 | 0 | 1 |
| mapOrbitToArray(Orbit, PositionAngle, double[], double[]) | | 100% | | 100% | 0 | 3 | 0 | 17 | 0 | 1 |
| mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| mapArrayToOrbit(RealFieldElement[], RealFieldElement[], PositionAngle, FieldAbsoluteDate, RealFieldElement, Frame) | | 100% | | 100% | 0 | 2 | 0 | 3 | 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 |