ObserverSatellite

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total27 of 11075%1 of 475%21022418
getOffsetToInertial(Frame, FieldAbsoluteDate, int, Map)190%n/a112211
getOffsetToInertial(Frame, AbsoluteDate, boolean)82273%1150%120501
lambda$getFieldPVCoordinatesProvider$0(FieldAbsoluteDate, Frame)25100%n/a010601
getFieldPVCoordinatesProvider(int, Map)16100%2100%020401
ObserverSatellite(String, PVCoordinatesProvider, QuadraticClockModel)8100%n/a010301
ObserverSatellite(String, PVCoordinatesProvider)7100%n/a010201
getPVCoordinatesProvider()3100%n/a010101
isSpaceBased()2100%n/a010101