| addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[]) |  | 96% |  | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
| initializeCachedAlpha(CalculusFieldElement, CalculusFieldElement, PositionAngleType) | | 94% | | 91% | 1 | 8 | 1 | 16 | 0 | 1 |
| getAlphaVDot() | | 94% | | 83% | 1 | 5 | 1 | 15 | 0 | 1 |
| getAlphaEDot() | | 94% | | 83% | 1 | 5 | 1 | 15 | 0 | 1 |
| getAlphaMDot() | | 94% | | 83% | 1 | 5 | 1 | 15 | 0 | 1 |
| initializeCachedAlpha(CalculusFieldElement, PositionAngleType) | | 92% | | 91% | 1 | 8 | 1 | 13 | 0 | 1 |
| getAlphaV() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
| getAlphaE() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
| getAlphaM() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 111 | 0 | 1 |
| FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) | | 100% | | 100% | 0 | 3 | 0 | 65 | 0 | 1 |
| computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 39 | 0 | 1 |
| FieldCircularOrbit(FieldOrbit) | | 100% | | 100% | 0 | 4 | 0 | 39 | 0 | 1 |
| initPosition() | | 100% | | n/a | 0 | 1 | 0 | 28 | 0 | 1 |
| nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 24 | 0 | 1 |
| FieldCircularOrbit(Field, CircularOrbit) | | 100% | | 100% | 0 | 2 | 0 | 23 | 0 | 1 |
| shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 18 | 0 | 1 |
| FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | 100% | 0 | 3 | 0 | 24 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| getHxDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getHyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getEDot() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| removeRates() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAlpha(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getAlphaDot(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLvDot() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getLEDot() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getLMDot() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| FieldCircularOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldCircularOrbit(Field, Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 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 |
| hasDerivatives() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 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 |
| 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 |
| getCachedPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |