1999-054A
The second 14F43M spacecraft, No. 2, was launched in 1999. It carried a Priroda-6 payload. Launch mass was 5920 kg. The satellite landed on Oct 21, but orbital data for the ejected engine were assigned to it after decay (corrected in the McDowell archive).
| Resurs F-1M | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1999 Sep 28 | 1100:05 | Launch by Soyuz-U | PL |
| T+1:57 Strapons sep | |||
| T+2:30 Fairing sep | |||
| T+4:44 Core sep 3.83km/s | |||
| T+4:54 Tail interstage sep 3.93km/s | |||
| 1108:49 | T+8:44 Stage 3 MECO 7.74km/s | ||
| 1108:52 | T+8:47 Stage 3 sep | ||
| 220 x 231 x 82.3 | |||
| 1999 Oct 21 | 0615? | Jettison KDU | |
| 0617? | Deorbit | ||
| 0625? | PO sep | ||
| 0635? | Reentry | ||
| 0646? | Landing | ||
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