| meanToHyperbolicEccentric(double, double) |   | 90% | | 87% | 2 | 9 | 2 | 23 | 0 | 1 |
| meanToEccentric(double, double, double) | | 90% | | 75% | 1 | 3 | 1 | 16 | 0 | 1 |
| shiftPVElliptic(double) | | 100% | | 100% | 0 | 2 | 0 | 39 | 0 | 1 |
| shiftPVHyperbolic(double) | | 100% | | 100% | 0 | 2 | 0 | 40 | 0 | 1 |
| addKeplerContribution(PositionAngle, double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| getEDot() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| getHxDot() | | 100% | | 83% | 1 | 4 | 0 | 11 | 0 | 1 |
| getHyDot() | | 100% | | 83% | 1 | 4 | 0 | 11 | 0 | 1 |
| getE() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| getPositionDS() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getVelocityDS() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| initEquinoctial() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| getADot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 3 | 0 | 4 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 3 | 0 | 4 | 0 | 1 |
| CartesianOrbit(Orbit) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getIDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| create6x6Identity() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| interpolate(AbsoluteDate, Stream) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| CartesianOrbit(TimeStampedPVCoordinates, Frame, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLv() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLEDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLM() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLMDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| writeReplace() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasDerivatives() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| initPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$interpolate$0(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |