AdvCAT: Secondary Vehicles

Lists values set for various parameters of each secondary object. This report is only valid after the AdvCAT computation has been performed.

Type: Fixed data. Intended to be used only with elements from this same data provider.

Availability: Reports

NameDimensionTypeDescription
EpochDateFormatReal NumberThe reference epoch for the object.
NormalDistanceUnitReal Number or TextIf the primary object is using a Fixed ellipsoid size, then the value is the size of the ellipsoid in the normal direction. If using another method for specifying the size, then the value is a description of the method being used to specify the size.
StatusUnitlessTextAn error status indicator.
StringIDUnitlessText The string identifier of the secondary object involved in the close approach event. If the object has no string identifier, then the value will be "Not Avail".
Cross-TrackDistanceUnitReal Number or TextIf the primary object is using a Fixed ellipsoid size, then the value is the size of the ellipsoid in the cross-track direction. If using another method for specifying the size, then the value is a description of the method being used to specify the size.
HardBodyRadiusSmallDistanceUnitReal NumberThe hard body radius value used for this object.
SourceUnitlessTextPlanetary Ephemeris data file type (i.e. JPL) and the actual files (i.e. DE430/LE430).
TypeUnitlessTextThe type of primary object.
NameUnitlessTextObject name that experienced an error.
TangentialDistanceUnitReal Number or TextIf the primary object is using a Fixed ellipsoid size, then the value is the size of the ellipsoid in the tangential direction. If using another method for specifying the size, then the value is a description of the method being used to specify the size.
NumberIDUnitlessText The number identifier of the secondary object involved in the close approach event. If the object has no number identifier, then the value will be "Not Avail".
SourceIDUnitlessTextThe identifier of the object as used by the ephemeris source for the object. For example, the identifier for objects that use a GPS sem or yuma file is PRN-##.
SSCUnitlessTextSSC number of the satellite with out of date TLE data for the date selected.
Start TimeDateFormatReal NumberThe start time of an interval.
Stop TimeDateFormatReal NumberThe stop time of an interval.