||3||08–08 08 ||Classification (U: unclassified, C: classified, S: secret) <ref>{{Cite web|url=https://ai-solutions.com/_help_Files/two-line_element_set_file.htm|title=Norad Two-Line Orbital Element Set File|website=ai-solutions.com|access-date=2019-09-03}}</ref>||U
|-
||4||10–11||[[International Designator]] (last two digits of launch year)||98
Line 69:
||8||21–32||[[Epoch (astronomy)|Epoch]] (day of the year and fractional portion of the day)||264.51782528
|-
||9||34–43||First derivative of [[mean motion]], aka; the ballistic coefficient <ref name="nasahelp">{{cite web|url=http://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/SSOP_Help/tle_def.html|archive-url=https://web.archive.org/web/20000301052035/http://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/SSOP_Help/tle_def.html|url-status=dead|archive-date=1 March 2000|title=NASA, ''Definition of Two-line Element Set Coordinate System''|publisher=Spaceflight.nasa.gov|access-date=28 November 2014}}</ref>||-.00002182
|-
||10||45–52||Second derivative of [[mean motion]] (decimal point assumed) <ref name="nasahelp" />||00000-0
|-
||11||54–61||Drag[[BSTAR|B*]], the drag term, akaor radiation pressure coefficient or [[BSTAR]] (decimal point assumed) <ref name="nasahelp"/>||-11606-4
|-
||12||63–63||Ephemeris type (internalalways usezero; only - always zeroused in distributedundistributed TLE data) <ref>{{Cite web|url=https://celestrak.com/columns/v04n03/|title=CelesTrak: "FAQs: Two-Line Element Set Format"|website=celestrak.com|access-date=2019-09-03}}</ref>||0
|-
||13||65–68||Element set number. Incremented when a new TLE is generated for this object. <ref name="nasahelp"/>||292
