Thursday, August 7, 1997
Nadezhda 2
1990-017A
The second named Nadezhda was launched in Feb 1990.
| Nadezhda (F2) | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Feb 27 | 2059:42 | Launch by Kosmos-3M | PL |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| T+2:12 St 2 burn 59km | |||
| T+2:27 Fairing 76km | |||
| 2108? | T+8:03 St 2 MECO 150 km | 150 x 1003? x 83 | |
| T+1:02:19 St 2 MES2 | |||
| T+1:02:30 St 2 MECO2 | |||
| 2203? | T+1:02:50 St 2 sep | ||
| 1996 Feb | KOSPAS-5 decommissioned | ||
Tuesday, August 5, 1997
Kosmos 455
1971-097A
DS-P1-Yu No. 54 was launched in Nov 1971 from Plesetsk. It was another subgroup 1 DS-P1-Yu mission.
| Kosmos-455 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Nov 17 | 1110 | Launch by 11K63 | PL |
| 1112 | Stage 2 burn | ||
| 1117? | Stage 2 sep | ||
| 1971 Nov 19 | 2130 | 92.19 272 x 491 x 71.0 (RAE) | |
| 1972 Feb 1 | 91.46 259 x 433 x 71.0 (RAE) | ||
| 1972 Apr 5 | End of operations | ||
| 1972 Apr 9 | 0028? | Reentered | |
Kosmos 247
1968-088A
Zenit-2 No. 65 was launched on 1968 Oct 11. Landing was 50 km N of Tselinograd at 51 14 N 71 17 E.
| Kosmos-247 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1968 Oct 11 | 1205 | Launch by 11A57 | NIIP-53 LC41/1 |
| 1210 | Blok-I burn | ||
| 1214 | Blok-I sep | ||
| 89.9 205 x 362 x 65.4 (TASS) | |||
| 1750 | 89.97 200 x 344 x 65.4 | ||
| 1968 Oct 12 | 0930? | 89.94 199 x 345 x 65.39 (RAE) | |
| 1968 Oct 16 | 0845 | 89.87 198 x 337 x 65.4 | |
| 1968 Oct 19 | 0537? | Deorbit | |
| 0543? | PO sep | ||
| 0602 | Landed | ||
Sunday, August 3, 1997
Kosmos 1552
1984-045A
This was the second Terilen flight. The operational orbit was reached after 3 days in the low perigee insertion orbit.
| Kosmos-1552 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1984 May 14 | 1400 | Launch by Soyuz | Baikonur |
| 1409 | Blok I sep | ||
| 1984 May 14 | 89.5 184x315x64.94 | ||
| 1984 May 15 | 197x316x64.9 | ||
| 1984 May 16 | 183x322x64.9 | ||
| 1984 May 17 | 1255? | Raise peri | |
| 1984 May 17 | 225x311x64.9 | ||
| 1984 May 25 | 224x316x64.9 | ||
| 1984 Oct 18 | 236x327x64.9 | ||
| 1984 Oct 21 | 234x322x64.9 | ||
| 1984 Nov 1 | 230x311x64.9 | ||
| 1984 Nov 2 | 229x307x64.9 | ||
| 1984 Nov 3 | |||
| 0904? | Deorbit (fiducial) | ||
| 0928? | Entry | ||
Kosmos 382
1970-103A
The second L-1E test flight was 7K-L1E No. 2, launched in Dec 1970 as Kosmos-382. It may have carried a supplementary ion engine experiment since the orbital eccentricity was observed to change slowly up to Feb 1971.
Several objects were cataloged in orbit with Kosmos-382. Objects E, F and G were ejected into the 160 minute orbit prior to burn 3. They were tracked later in high apogee orbits which continued to become more eccentric, and were presumably being affected by radiation pressure.
Objects B and C are believed to be the SOZ motors; they were ejected into the 160 minute orbit around the time of burn 3.
Object D was released after burn 3 into the final orbit, but was strongly affected by radiation pressure and decay and has a low RCS. It may be an insulation panel of some kind.
Three in-orbit burns had 982, 285 and 1311 m/s. There were seven burns in total.
| Kosmos-382 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1970 Dec 2 | 1700:00 | Launch by Proton-K | KB |
| 1702 | Stage 2 | ||
| 1705 | Stage 2 cutoff | ||
| 1705 | Stage 3 burn | ||
| 1709 | Stage 3 cutoff | -1350? x 200 x 51.6 | |
| 1715? | Blok-D burn 1 | ||
| 1717? | Blok-D MECO-1 | ||
| 190 x 300 km | |||
| Burn 1 (simulated LOI-1) | |||
| 1723? | Stage 3 reentry | ||
| 1752 | Blok-D MES-2 | ||
| 1755 | Blok-D MECO-2 | 303 x 5038 x 51.6 | |
| 1970 Dec 3 | 1100 | 142.77 303 x 5038 x 51.57 (TLE) | |
| 1148 | Burn 3 tweak 3m/s | ||
| 1970 Dec 4 | 1148 | Burn 4 tweak 2m/s | |
| 1970 Dec 4 | 1300 | 142.88 303 x 5046 x 51.53 (TLE) | |
| 1970 Dec 4 | 142.98 318 x 5040 x 51.55 (TLE) | ||
| 1636 | Burn 5 orbit tweak 19m/s | ||
| 1970 Dec 5 | 144.11 408 x 5045 x 51.53 (TLE) | ||
| 1970 Dec 6 | 1856? | Orbit change over 71E 50N? | 158.99 1616 x 5071 x 51.55 |
| Burn 6 (simulated LOI-2) | |||
| 103E,F,G sep to 160 min orbit, decaying | ||
| 1970 Dec 7 | 1554? | MES-7 | |
| 1970 Dec 7 | 1555 | Burn 7 over 82E 50N | |
| Burn 7 (simulated DOI) | ||
| 1554? | SOZ jettison (B,C) | 1615 x 5082 x 51.6 | |
| 1557? | Burn 7 cutoff | 171.06 2577 x 5082 x 55.87 | |
| 103D sep to 172 min orbit, decaying | |||
| 1970 Dec 15 | 1955 | 171.04 2581 x 5077 x 55.87 | |
| 1970 Dec 29 | 1144 | 171.03 2585 x 5012 x 55.87 | |
| 1971 Feb 10 | End of ion engine test? | ||
| 1992 Jul 22 | 171.00 2389 x 5265 x 55.85 | ||
| 1998 Apr 30 | 171.00 2376 x 5278 x 55.88 | ||
May 13,2026
https://planet4589.org/space/jsr/back/news.855.txt
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