Progress M-33 was successfully launched at 23:20:38.104 UTC. EFG after processing of trajectory measurements on 1st and 2nd orbits: Orbit 2 20/11/1996 00:37:59.954 UTC 6491.40816 km -1121.19795 km 0.00000 km 0.704812441 km/s 4.28989898 km/s 6.10528816 km/s nodal period - 1h 28min 38.570 s semimaj. axis - 6595.5333 km eccentr. - 0.004733894 incl. - 51.6655 deg arg. of perig. - 75.39722 deg RAAN (B1950) - 59.2684 deg Hmin - 192.087 km Hmax - 252.368 km Nominal parameters of manoeuvres and nominal state vectors at MECO #1 and MECO #2 1st burn 02:29:06 UTC 21.62 m/s 52.65 s Vector at MECO #1 Orbit 3 20/11/1996 02:59:58.6452 UTC -5.439667 km 2.023059 km -3.159132 km 0.678168 km/s -5.662330 km/s -4.848236 km/s 2nd burn 03:47:59 UTC 18.97 m/s 45.88 s Vector at MECO #2 Orbit 4 20/11/1996 03:48:44.8769 UTC 4.893667 km -1.659770 km 4.160508 km -0.946513 km/s 6.454054 km/s 3.634797 km/s All the best, Vladimir Agapov.