OMMFile

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total11 of 20695%1 of 250%129149028
generateKeplerianOrbit()113274%1150%121601
generateTLE()48100%n/a010501
OMMFile()9100%n/a010301
generateSpacecraftState()8100%n/a010101
setTLERelatedParametersComment(List)7100%n/a010201
generateCartesianOrbit()6100%n/a010101
setbStar(double)5100%n/a010201
setMeanMotionDot(double)5100%n/a010201
setMeanMotionDotDot(double)5100%n/a010201
getCoordinateSystem()5100%n/a010101
setMeanMotion(double)4100%n/a010201
setEphemerisType(int)4100%n/a010201
setClassificationType(char)4100%n/a010201
setNoradID(Integer)4100%n/a010201
setElementSetNo(String)4100%n/a010201
setRevAtEpoch(int)4100%n/a010201
getBStar()4100%n/a010101
getMeanMotionDot()4100%n/a010101
getMeanMotionDotDot()4100%n/a010101
getTLERelatedParametersComment()4100%n/a010101
getTimeSystem()4100%n/a010101
getMetaData()3100%n/a010101
getMeanMotion()3100%n/a010101
getEphemerisType()3100%n/a010101
getClassificationType()3100%n/a010101
getNoradID()3100%n/a010101
getElementSetNumber()3100%n/a010101
getRevAtEpoch()3100%n/a010101