OrbitElementsType.new OrbitElementsType() {...}

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 106100%0 of 0n/a030603
toRawElements(TimeStampedPVCoordinates, Frame, OneAxisEllipsoid, double)57100%n/a010401
toCartesian(AbsoluteDate, double[], OneAxisEllipsoid, double)41100%n/a010101
{...}8100%n/a010101