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Line 65:
||6||15–17||[[International Designator]] (piece of the launch)||A
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||7||19–20||[[Epoch (astronomy)|Epoch]]
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||8||21–32||[[Epoch (astronomy)|Epoch]] (day of the year and fractional portion of the day)||264.51782528
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||9||34–43||First
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||10||45–52||Second
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||11||54–61||Drag
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||12||63–63||Ephemeris type (internal use only - always zero in distributed 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
Line 79:
||13||65–68||Element set number. Incremented when a new TLE is generated for this object. <ref name="nasahelp"/>||292
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||14||69–69||[[Checksum]] ([[
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Line 98:
||3||09–16||[[Orbital inclination|Inclination]] (degrees)||51.6416
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||4||18–25||[[Right ascension of the ascending node
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||5||27–33||[[Orbital eccentricity|Eccentricity]] (decimal point assumed)||0006703
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||6||35–42||[[Argument of perigee
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||7||44–51||[[Mean
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||8||53–63||[[Mean
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||9||64–68||Revolution number at epoch (revolutions)||56353
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