| meanToHyperbolicEccentric(RealFieldElement, RealFieldElement) |   | 92% | | 87% | 2 | 9 | 2 | 23 | 0 | 1 |
| meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement) | | 92% | | 75% | 1 | 3 | 1 | 16 | 0 | 1 |
| shiftPVElliptic(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 42 | 0 | 1 |
| shiftPVHyperbolic(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 41 | 0 | 1 |
| addKeplerContribution(PositionAngle, RealFieldElement, RealFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| getE() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| getHxDot() | | 100% | | 83% | 1 | 4 | 0 | 11 | 0 | 1 |
| getHyDot() | | 100% | | 83% | 1 | 4 | 0 | 11 | 0 | 1 |
| getEDot() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| FieldCartesianOrbit(FieldOrbit) | | 100% | | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
| getPositionDS() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getVelocityDS() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| FieldCartesianOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| initEquinoctial() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getADot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| create6x6Identity() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| shiftedBy(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getIDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| interpolate(FieldAbsoluteDate, Stream) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldCartesianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
| static {...} | | 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(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |