| computeJacobianEccentricWrtCartesian() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| shiftPV(CalculusFieldElement) |  | 100% | | 100% | 0 | 2 | 0 | 20 | 0 | 1 |
| addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| getPVDerivatives() | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| getE() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| getHxDot() | | 100% | | 83% | 1 | 4 | 0 | 12 | 0 | 1 |
| getHyDot() | | 100% | | 83% | 1 | 4 | 0 | 12 | 0 | 1 |
| getEDot() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 11 | 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 |
| FieldCartesianOrbit(Field, CartesianOrbit) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getADot() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| FieldCartesianOrbit(FieldOrbit) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| withFrame(Frame) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| create6x6Identity() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getIDot() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| shiftedBy(CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldCartesianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldCartesianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldCartesianOrbit(Field, Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| shiftedBy(double) | | 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 |
| initPosition() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasNonKeplerianAcceleration() | | 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 |
| computeJacobianTrueWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |