| equinoctialToPosition(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, double) |  | 0% | | n/a | 1 | 1 | 24 | 24 | 1 | 1 |
| FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates, Frame, double) |  | 97% | | 83% | 1 | 4 | 2 | 61 | 0 | 1 |
| FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) | | 95% | | 85% | 2 | 10 | 2 | 46 | 0 | 1 |
| addKeplerContribution(PositionAngle, double, RealFieldElement[]) | | 96% | | 75% | 1 | 4 | 1 | 14 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 57 | 0 | 1 |
| computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 34 | 0 | 1 |
| interpolate(FieldAbsoluteDate, Stream) | | 100% | | 100% | 0 | 7 | 0 | 39 | 0 | 1 |
| nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 23 | 0 | 1 |
| shiftedBy(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 17 | 0 | 1 |
| meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | 75% | 1 | 3 | 0 | 17 | 0 | 1 |
| FieldEquinoctialOrbit(FieldOrbit) | | 100% | | 100% | 0 | 2 | 0 | 19 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| getLMDot() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| getLEDot() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| eccentricToTrue(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| trueToEccentric(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getIDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getEDot() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| eccentricToMean(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| normalizeAngle(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getL(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getLDot(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldEquinoctialOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasDerivatives() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| static {...} | | 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 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHxDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHyDot() | | 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 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |