EcksteinHechlerOrbitalState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 65100%0 of 0n/a0701607
createOrekitOrbit()30100%n/a010601
createPropagator()11100%n/a010201
EcksteinHechlerOrbitalState(AbsoluteDate, AveragedCircularWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider)9100%n/a010301
toOsculatingOrbit()8100%n/a010201
getAveragedElements()3100%n/a010101
getOrbitType()2100%n/a010101
getPositionAngleType()2100%n/a010101