| initializeCachedL(double, double, PositionAngleType) |   | 94% | | 91% | 1 | 8 | 1 | 16 | 0 | 1 |
| getLvDot() | | 93% | | 75% | 1 | 4 | 1 | 13 | 0 | 1 |
| getLEDot() | | 93% | | 75% | 1 | 4 | 1 | 13 | 0 | 1 |
| getLMDot() | | 93% | | 75% | 1 | 4 | 1 | 13 | 0 | 1 |
| getLv() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
| getLE() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
| getLM() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 52 | 0 | 1 |
| EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) | | 100% | | 100% | 0 | 3 | 0 | 55 | 0 | 1 |
| computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 31 | 0 | 1 |
| nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| initPosition() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 23 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | 100% | 0 | 3 | 0 | 24 | 0 | 1 |
| computeKeplerianLDot(PositionAngleType, double, double, double, double, double, PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| EquinoctialOrbit(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getIDot() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| removeRates() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| addKeplerContribution(PositionAngleType, double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getL(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getLDot(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| initializeCachedL(double, PositionAngleType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| writeReplace() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| eccentricToTrue(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| trueToEccentric(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| meanToEccentric(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| eccentricToMean(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHxDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCachedPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |