First two of five manoeuvres of Progress are scheduled finally now: 1st manoeuvre 2nd manoeuvre Orbit #3 #4 Date 1997/12/20 1997/12/20 Time 12:26:32 UTC 13:17:43 UTC dV 26.74 m/s 23.3 m/s Yaw 340.94 deg 17.94 deg Pitch -2.07 deg -1.79 deg Burn duration 65.1sec 56.3sec Nominal EFG vectors after each manoeuvre are: Date 1997/12/20 1997/12/20 Time, UTC 12:27:37.102 13:18:39.249 X, km -5179.336 4290.516 Y, km 871.902 559.4346 Z, km -4013.295 5036.937 Vx, km/s 1.949139 -2.711303 Vy, km/s -6.099687 6.783228 Vz, km/s -3.869071 1.520260 Launch mass of the Progress was 7195 kg. Best regards, Vladimir Agapov. -- Vladimir M. Agapov | Ballistic Center of Moscow, Russia | the Keldysh Institute of Applied Mathematics RAN | Moscow, Russia e-mail: avm@kiam1.rssi.ru | tel +7-095-333-8067 (work), fax +7-095-333-6334