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README@ 2009

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Last change on this file since 2009 was 1719, checked in by cmv, 24 years ago
Adapted to version 3.5 xephem cmv 22/10/2001
File size: 672 bytes

Rev	Line
[1457]	1	This library contains the basic ephemeris code.
	2
	3	Earth satellite orbit propagation is based on the NORAD SGP4/SDP4 code, as
	4	converted from the orginal FORTRAN to C by Magnus Backstrom. The paper
	5	"Spacetrack Report Number 3: Models for Propagation of NORAD Element Sets"
	6	describes the calculations.
	7	See http://www.celestrak.com/NORAD/documentation/spacetrk.pdf.
	8	He following files implement this package:
	9	actan.c
	10	deep.c
	11	deepconst.h
	12	satlib.h
	13	satspec.h
	14	sattypes.h
	15	sdp4.c
	16	sgp4.c
	17	thetag.c
	18	vector.h
	19
	20	! For RCS Only -- Do Not Edit
[1719]	21	! @(#) $RCSfile: README,v $ $Date: 2001-10-22 12:08:25 $ $Revision: 1.2 $ $Name: not supported by cvs2svn $

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