Hello, I would like to calculate the lat/lon of orbiting bodies from TLE's. Can someone point me in the right direction to find a formula for achieving this? Thanks in advance. c. ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www.satellite.eu.org/seesat/seesatindex.html
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