RtcmOrbitCorrectionData

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 17100%0 of 0n/a050805
setGnssIod(int)4100%n/a010201
setOrbitCorrection(OrbitCorrection)4100%n/a010201
RtcmOrbitCorrectionData()3100%n/a010201
getGnssIod()3100%n/a010101
getOrbitCorrection()3100%n/a010101