OrbitElementsType.new OrbitElementsType() {...}

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 48100%0 of 0n/a030403
toRawElements(TimeStampedPVCoordinates, Frame, OneAxisEllipsoid, double)21100%n/a010201
toCartesian(AbsoluteDate, double[], OneAxisEllipsoid, double)19100%n/a010101
{...}8100%n/a010101