| CircularOrbit(TimeStampedPVCoordinates, Frame, double) |   | 97% | | 75% | 1 | 3 | 2 | 63 | 0 | 1 |
| CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) | | 93% | | 83% | 2 | 9 | 2 | 41 | 0 | 1 |
| addKeplerContribution(PositionAngle, double, double[]) | | 95% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 80 | 0 | 1 |
| interpolate(AbsoluteDate, Stream) | | 100% | | 100% | 0 | 7 | 0 | 42 | 0 | 1 |
| computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 35 | 0 | 1 |
| CircularOrbit(Orbit) | | 100% | | 100% | 0 | 4 | 0 | 37 | 0 | 1 |
| nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 24 | 0 | 1 |
| shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| meanToEccentric(double, double, double) | | 100% | | 75% | 1 | 3 | 0 | 15 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, TimeStampedPVCoordinates, Frame, double) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| eccentricToTrue(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| trueToEccentric(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getHxDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getHyDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getAlphaMDot() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getAlphaEDot() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getAlpha(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getAlphaDot(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| eccentricToMean(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAlphaM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getAlphaE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLMDot() | | 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 |
| getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCircularEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCircularExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCircularEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCircularEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAlphaV() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAlphaVDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRightAscensionOfAscendingNode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRightAscensionOfAscendingNodeDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |