OrbitType.new OrbitType() {...}

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	33 of 416	92%	1 of 12	91%	1	14	7	62	0	8
mapOrbitToArray(FieldOrbit, PositionAngle, CalculusFieldElement[], CalculusFieldElement[])		56%		50%	1	2	7	18	0	1
getDrivers(double, Orbit, PositionAngle)		100%		n/a	0	1	0	11	0	1
mapOrbitToArray(Orbit, PositionAngle, double[], double[])		100%		100%	0	2	0	18	0	1
mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame)		100%		100%	0	2	0	6	0	1
mapArrayToOrbit(CalculusFieldElement[], CalculusFieldElement[], PositionAngle, FieldAbsoluteDate, CalculusFieldElement, Frame)		100%		100%	0	2	0	6	0	1
convertType(Orbit)		100%		100%	0	2	0	1	0	1
convertType(FieldOrbit)		100%		100%	0	2	0	1	0	1
{...}		100%		n/a	0	1	0	1	0	1