| EquinoctialOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) |  | 0% | | 0% | 5 | 5 | 18 | 18 | 1 | 1 |
| toString() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) |  | 93% | | 50% | 1 | 2 | 1 | 24 | 0 | 1 |
| addKeplerContribution(PositionAngle, double, double[]) | | 97% | | 75% | 1 | 4 | 1 | 14 | 0 | 1 |
| EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) | | 96% | | 83% | 1 | 5 | 1 | 17 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 51 | 0 | 1 |
| initPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 27 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 23 | 0 | 1 |
| interpolate(AbsoluteDate, Collection) | | 100% | | 100% | 0 | 3 | 0 | 16 | 0 | 1 |
| meanToEccentric(double) | | 100% | | 75% | 1 | 3 | 0 | 17 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| eccentricToTrue(double) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| EquinoctialOrbit(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLM() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getL(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 1 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |