| normalizeAngle(RealFieldElement, RealFieldElement) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| meanToHyperbolicEccentric(RealFieldElement, RealFieldElement) |  | 92% | | 87% | 2 | 9 | 2 | 23 | 0 | 1 |
| FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement) | | 96% | | 91% | 2 | 15 | 2 | 56 | 0 | 1 |
| addKeplerContribution(PositionAngle, RealFieldElement, RealFieldElement[]) | | 95% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
| computeJacobianMeanWrtCartesianElliptical() | | 100% | | n/a | 0 | 1 | 0 | 84 | 0 | 1 |
| computeJacobianMeanWrtCartesianHyperbolic() | | 100% | | n/a | 0 | 1 | 0 | 88 | 0 | 1 |
| FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement, boolean) | | 100% | | 100% | 0 | 5 | 0 | 64 | 0 | 1 |
| interpolate(FieldAbsoluteDate, Stream) | | 100% | | 100% | 0 | 7 | 0 | 47 | 0 | 1 |
| computePVWithoutA() | | 100% | | 100% | 0 | 3 | 0 | 38 | 0 | 1 |
| meanToEllipticEccentric(RealFieldElement, RealFieldElement) | | 100% | | 100% | 0 | 7 | 0 | 28 | 0 | 1 |
| nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
| shiftedBy(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 16 | 0 | 1 |
| computeJacobianTrueWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| computeJacobianTrueWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
| getHxDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getHyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getMeanAnomalyDot() | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getEccentricAnomalyDot() | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
| eMeSinE(RealFieldElement, RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| computeJacobianEccentricWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| computeJacobianEccentricWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| ellipticEccentricToTrue(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| trueToEllipticEccentric(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| hyperbolicEccentricToTrue(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| trueToHyperbolicEccentric(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMeanAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEccentricAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getLvDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getLEDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getLMDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getAnomaly(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getAnomalyDot(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 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 |
| FieldKeplerianOrbit(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| hyperbolicEccentricToMean(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| ellipticEccentricToMean(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasDerivatives() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEDot() | | 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 |
| getPerigeeArgument() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPerigeeArgumentDot() | | 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 |
| getTrueAnomaly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTrueAnomalyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |