OrbitElementsType.new OrbitElementsType() {...}

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 77100%0 of 0n/a030503
toRawElements(TimeStampedPVCoordinates, Frame, OneAxisEllipsoid, double)39100%n/a010301
toCartesian(AbsoluteDate, double[], OneAxisEllipsoid, double)30100%n/a010101
{...}8100%n/a010101