Progress M1-2 was successfully launched at 20:08:02.001 UTC from LC1 of Baykonur. Determined EFG vector after the first orbit measurements processing is very close to the nominal one: 2000/04/25 20:16:51.18 UTC 338.511 km 4116.687 km 5093.876 km -7.458334 km/s -0.405747 km/s 0.821403 km/s It's a good chance to visually observ early orbits of Progress prior to the first series of manoeuvres. Vladimir Agapov. ----------------------------------------------------------------- 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
This archive was generated by hypermail 2b29 : Tue Apr 25 2000 - 13:54:31 PDT