SGP4OrbitalState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 15498%0 of 0n/a114136114
getMu()20%n/a111111
createTLE()50100%n/a010901
of(TLE, Frame)28100%n/a010501
SGP4OrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle, Frame, TimeScale)12100%n/a010401
SGP4OrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle, DataContext)11100%n/a010301
computeMeanMotion(double)11100%n/a010201
computeSemiMajorAxis(TLE)10100%n/a010201
createPropagator()8100%n/a010201
toOsculatingOrbit()7100%n/a010201
SGP4OrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle)6100%n/a010201
getAveragedElements()3100%n/a010101
getTleMu()2100%n/a010101
getOrbitType()2100%n/a010101
getPositionAngleType()2100%n/a010101