2002-045A
M1-9 (258) was launched in Sep 2002 on mission 9P. Launch mass was 7440 kg. It used fairing 11S517A2 No. 57 and launch vehicle 11A511U-FG No. E15000-003. Over a long 4-day approach the Kurs system was tested out, stationkeeping 10 to 30 km from ISS.
| Progress M1-9 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2002 Sep 25 | 1658:24 | Launch by Soyuz-FG | KB |
| 1700:22 | St 1 sep | ||
| 1700:57 | GO sep | ||
| 1703:11 | St 2 sep | ||
| 1703:22 | KhO sep | ||
| 1707:08 | St 3 MECO | ||
| 1707:12 | Blok-I sep | ||
| 1939:02 | DV1 458s 30m/s | ||
| 2126:13 | DV2 395s 26m/s | ||
| 2002 Sep 26 | 1832:05 | DV3 5s 2m/s | |
| 2002 Sep 27 | 1455:18 | DV4 TCM, 413s, 28m/s Kurs test at 30 km to ISS | |
| 1533:09 | DV5 TCM 297s 20m/s | ||
| 2002 Sep 28 | 1719:10 | DV6 TCM 8s 0.5m/s | |
| 2002 Sep 29 | 1453:23 | DV7 TCM 31s 12m/s | |
| 1539:29 | DV8 TCM 1s 0.3m/s | ||
| 1632s | Flyaround 400m | ||
| 1641s | Stationkeeping 170m | ||
| 1655s | Final approach | ||
| 1700:54 | Docking with Zvezda rear port | ||
| 2146 | HO to Zvezda | ||
| 2002 Oct 18 | 0825 | Reboost 4.4m/s | |
| 2003 Feb 1 | 1600:54 | Undocking (NK) | |
| 1602:00 | Undocked from Zvezda | ||
| 1910:00 | Deorbit burn 97.4m/s 3:00, 49 32N 33 56E | ||
| 1912:59 | Deorbit cutoff | 88.92 58 x 383 x 51.6 | |
| 1946:50 | Entry, 105 km 48 26S 154 23E | ||
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