| FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) |   | 97% |   | 75% | 1 | 3 | 2 | 64 | 0 | 1 |
| FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) |   | 93% |   | 83% | 2 | 9 | 2 | 40 | 0 | 1 |
| addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[]) |  | 96% |   | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
| computeJacobianMeanWrtCartesian() |  | 100% | | n/a | 0 | 1 | 0 | 111 | 0 | 1 |
| computePVWithoutA() |  | 100% |  | 100% | 0 | 2 | 0 | 39 | 0 | 1 |
| FieldCircularOrbit(FieldOrbit) |  | 100% |  | 100% | 0 | 4 | 0 | 38 | 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 | 22 | 0 | 1 |
| shiftedBy(CalculusFieldElement) |  | 100% |  | 100% | 0 | 2 | 0 | 18 | 0 | 1 |
| meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% |   | 75% | 1 | 3 | 0 | 15 | 0 | 1 |
| toOrbit() |  | 100% |  | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| getHxDot() |  | 100% |  | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getHyDot() |  | 100% |  | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| toString() |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| initPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getAlphaMDot() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getEquinoctialExDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getEquinoctialEyDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getAlphaEDot() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getHx() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getHy() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| removeRates() |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getEDot() |  | 100% |  | 100% | 0 | 2 | 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, Frame, FieldAbsoluteDate, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| eccentricToMean(CalculusFieldElement, CalculusFieldElement, 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 |
| getAlphaM() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 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 |
| getAlphaE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 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 |
| 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 |
| getAlphaV() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAlphaVDot() | | 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 |
| hasRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCachedPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |