OMMFile

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	11 of 201	94%	1 of 2	50%	1	27	1	48	0	26
generateKeplerianOrbit()		74%		50%	1	2	1	6	0	1
generateTLE()		100%		n/a	0	1	0	6	0	1
OMMFile()		100%		n/a	0	1	0	3	0	1
generateSpacecraftState()		100%		n/a	0	1	0	1	0	1
setTLERelatedParametersComment(List)		100%		n/a	0	1	0	2	0	1
generateCartesianOrbit()		100%		n/a	0	1	0	1	0	1
setbStar(double)		100%		n/a	0	1	0	2	0	1
setMeanMotionDot(double)		100%		n/a	0	1	0	2	0	1
setMeanMotionDotDot(double)		100%		n/a	0	1	0	2	0	1
setMeanMotion(double)		100%		n/a	0	1	0	2	0	1
setEphemerisType(int)		100%		n/a	0	1	0	2	0	1
setClassificationType(char)		100%		n/a	0	1	0	2	0	1
setNoradID(Integer)		100%		n/a	0	1	0	2	0	1
setElementSetNo(String)		100%		n/a	0	1	0	2	0	1
setRevAtEpoch(int)		100%		n/a	0	1	0	2	0	1
getBStar()		100%		n/a	0	1	0	1	0	1
getMeanMotionDot()		100%		n/a	0	1	0	1	0	1
getMeanMotionDotDot()		100%		n/a	0	1	0	1	0	1
getTLERelatedParametersComment()		100%		n/a	0	1	0	1	0	1
getMetaData()		100%		n/a	0	1	0	1	0	1
getMeanMotion()		100%		n/a	0	1	0	1	0	1
getEphemerisType()		100%		n/a	0	1	0	1	0	1
getClassificationType()		100%		n/a	0	1	0	1	0	1
getNoradID()		100%		n/a	0	1	0	1	0	1
getElementSetNumber()		100%		n/a	0	1	0	1	0	1
getRevAtEpoch()		100%		n/a	0	1	0	1	0	1