Content deleted Content added
m Add detail to the RAAN parameters |
m add missing units-of-measurement to table from the [12] NASA source |
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Line 74:
||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 derivative of [[mean motion]]; the ballistic coefficient (rev/day, per day)<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
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||10||45–52||Second derivative of [[mean motion]] (rev/day³, decimal point assumed)<ref name="nasahelp" />||00000-0
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||11||54–61||[[BSTAR|''B''*]], the drag term, or radiation pressure coefficient (units of 1/(Earth radii), decimal point assumed)<ref name="nasahelp"/>||-11606-4
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||12||63||Ephemeris type (always zero; only used in undistributed TLE data)<ref>{{Cite web|url=https://celestrak.com/columns/v04n03/|title=CelesTrak: "FAQs: Two-Line Element Set Format" |first=T. S. |last=Kelso |website=celestrak.com|access-date=2019-09-03}}</ref>||0
Line 105:
||4||18–25||[[Right ascension of the ascending node]] (degrees), in the [[Earth-centered inertial|ECI reference frame]], measured from the [[vernal point]]||247.4627
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||5||27–33||[[Orbital eccentricity|Eccentricity]] (unitless, decimal point assumed)||0006703
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||6||35–42||[[Argument of perigee]] (degrees)||130.5360
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