> But sin(Launch Azimuth) = cos(i) / cos(lat) (90 degrees when i=lat) > so here Launch Azimuth is 45 degrees. Right, this is the inertial launch azimuth. Because the launch site has a velocity component (the Earth rotates with 0.409 km/s to the east at KSC) the actual launch azimuth would be around 2 deg more to the north, for a coplanar launch. Cheers, Sebastian ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www2.satellite.eu.org/sat/seesat/seesatindex.html
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