GE-1A 35725 x 217 km 1 26554U 00059A 00275.97042671 -.00000238 00000-0 00000-0 0 25 2 26554 48.5427 349.9203 7291408 0.0363 0.1310 2.28521338 06 GE-1A Blok-DM r 35823 x 7394 km 1 26557U 00059D 00276.42872861 -.00000208 00000-0 00000-0 0 17 2 26557 15.9434 352.8128 5078951 359.3738 336.5518 1.85446958 28 Since the Blok-DM rocket put the payload into GEO transfer orbit, how does it end up in a 15.9 degree inclination orbit with a perigee at 7394 km while the payload is at 48.5 degree inclination and a perigee of 217 km? This does not look logical to me. Ron Lee ----------------------------------------------------------------- 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/seesat/seesatindex.html
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