| toString() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) |  | 86% | | 83% | 2 | 8 | 2 | 21 | 0 | 1 |
| meanToHyperbolicEccentric(double, double) | | 91% | | 81% | 3 | 9 | 1 | 22 | 0 | 1 |
| addKeplerContribution(PositionAngle, double, double[]) | | 97% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
| getHx() | | 90% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| getHy() | | 90% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| computeJacobianMeanWrtCartesianElliptical() | | 100% | | n/a | 0 | 1 | 0 | 73 | 0 | 1 |
| computeJacobianMeanWrtCartesianHyperbolic() | | 100% | | n/a | 0 | 1 | 0 | 88 | 0 | 1 |
| meanToEllipticEccentric(double) | | 100% | | 100% | 0 | 6 | 0 | 26 | 0 | 1 |
| KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) | | 100% | | 100% | 0 | 2 | 0 | 27 | 0 | 1 |
| interpolate(AbsoluteDate, Collection) | | 100% | | 100% | 0 | 3 | 0 | 24 | 0 | 1 |
| initPVCoordinatesElliptical(Vector3D, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 15 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| initPVCoordinatesHyperbolic(Vector3D, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| computeJacobianTrueWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| computeJacobianTrueWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| getEccentricAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| computeJacobianEccentricWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| computeJacobianEccentricWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| eMeSinE(double) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| ellipticEccentricToTrue(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMeanAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| hyperbolicEccentricToTrue(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAnomaly(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 1 | 0 | 1 |
| KeplerianOrbit(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| writeReplace() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPerigeeArgument() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRightAscensionOfAscendingNode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTrueAnomaly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |