Microsoft Word - AIAARevisiting Spacetrack Report 3 Rev 2.docx - Culmination - Document - PDFSEARCH.IO

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Date: 2012-08-06 14:16:05 Simplified 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.docx Add to Reading List Source URL: celestrak.com Download Document from Source Website File Size: 651,92 KB Share Document on Facebook

	ANALYSIS OF THE MEGHA-TROPIQUES TRAJECTORY. DETERMINATION OF RENDEZ-VOUS CONDITIONS WITH THE TERRA SATELLITE. Michel Capderou(1) , Florent Deleflie(2) , and Olivier Chomette(1) Ecole Polytechnique, FPalaiseau, Mic DocID: 1fYaI - View Document
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	This is just Kepler’s third law, which says that the period of an orbit is proportional to the 3/2 power of its radius; 6378 km is the radius of the Earth. At an altitude ofkm, a satellite orbits the Earth once DocID: 11ACI - View Document
	Tech Note #2 December 12, 2001 DocID: 1Pe8 - View Document
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