Spaceflight Now reports that the launch time of ATV 1 has been moved 4 min later, to 2008 Mar 09 at 04:03 UTC: http://www.spaceflightnow.com/tracking/index.html Here are my revised elements and related information: Please Note: I estimate prediction time accuracy for the first couple of revs to be about 2 min; sky-track predictions could easily be off by several degrees, especially on high elevation passes. I would appreciate any information that would enable improving the accuracy of these elements; an official state vector would be ideal. The initial orbit is valid from approximately 04:20 to 05:05 UTC: ATV/ESC 14.5 5.0 0.0 3.0 v 136 X 260 km 1 71700U 08069.21209491 .00000000 00000-0 00000-0 0 09 2 71700 51.6000 172.3200 0094300 52.0000 180.3000 16.28160000 03 While in the initial orbit, ATV will remain attached to the Ariane 5's ESC upper stage, resulting in a stack about 14.5 m long, and mean diameter of about 5 m. Estimated standard visual magnitude is about 3 (1000 km range, 90 deg phase-angle). The circularized orbit is valid beginning shortly after 05:05 UTC: ATV 1 9.8 4.5 0.0 3.5 v 259 X 261 km 1 71700U 08069.21209492 .00000000 00000-0 00000-0 0 00 2 71700 51.6000 172.3200 0001000 52.0000 180.3000 16.05406000 06 The 4.7 m x 5.4 m upper stage will be in a similar orbit, until its de-orbit burn, at about 06:31 UTC, just west of Australia. Note: the epoch of both of the above element sets corresponds to first apogee, near the time of the circularization burn. Visibility from Europe On its first pass over Europe, the ATV/ESC stack is predicted to exit eclipse at about 04:28 UTC, about 149 km above 50.8 N, 13 E, as it approaches Eastern Europe. One rev later, at about 5:58 UTC, ATV and its ESC stage (now separated) will pass over the U.K., at about 51.5 N latitude, at an altitude of about 265 km. This will be near the start of civil twilight. Ted Molczan ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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