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Date: 2012-08-06 14:16:05Simplified perturbations models Two-line element set Orbital elements Orbit Epoch Equinox Air Force Space Command Ephemeris United States Space Surveillance Network Astrology Celestial mechanics Space | Microsoft Word - AIAARevisiting Spacetrack Report 3 Rev 2.docxAdd to Reading ListSource URL: celestrak.comDownload Document from Source WebsiteFile Size: 651,92 KBShare Document on Facebook |
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Derivation of the Relationship Between B * and n&[removed]by Ted Molczan, October 1999 Background During, my experience with the NORAD “2-line” orbital elements and the SGP and SGP4 orbit propagators, revealedDocID: 11SL8 - View Document | |
Tech Note #2 December 12, 2001DocID: 1Pe8 - View Document | |
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