1989-005A
| Kosmos-1992 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Jan 26 | 1536:00 | Launch by 11K65M | Plesetsk 41.47E |
| Stage 2 burn | |||
| 1544? | T+8 min Stage 2 MECO-1 | ||
| Stage 2 MES-2 | |||
| T+34min Stage 2 MECO-2 | |||
| 1610? | Stage 2 sep | ||
| 100.56 772x798x74.1 | |||
1989-005A
| Kosmos-1992 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Jan 26 | 1536:00 | Launch by 11K65M | Plesetsk 41.47E |
| Stage 2 burn | |||
| 1544? | T+8 min Stage 2 MECO-1 | ||
| Stage 2 MES-2 | |||
| T+34min Stage 2 MECO-2 | |||
| 1610? | Stage 2 sep | ||
| 100.56 772x798x74.1 | |||
1969-077A
Testing of the OGCh resumed in Sep 1969 with the flight of Kosmos-298.
| Kosmos-298 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1969 Sep 15 | 1600:00 | Launch by 8K69 | KB |
| 1602 | Stage 2 burn | ||
| 1605 | Stage 2 sep | 87.31 127 x 162 x 49.60 | |
| 1605 | Adapter sep | ||
| 1727? | Deorbit | ||
| 1731? | Impact near GTsP4? | ||
1970-104A
Zenit-4MK flight 4,Kosmos-383,was launched from Plesetsk in Dec 1970.
| Kosmos-383 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1970 Dec 3 | 1355:19 | Launch by 11A57 | PL |
| 1359 | Blok-I burn | ||
| 1403 | Blok-I sep | ||
| 1938 | 89.32 181 x 300 x 65.4 | ||
| 1970 Dec 4 | 1700 | 89.33 204 x 279 x 65.41 (RAE) | |
| 1970 Dec 7 | 0954 | 89.04 185 x 268 x 65.4 | |
| 1970 Dec 11 | 0846 | 88.80 163 x 266 x 65.5 | |
| Orbit raise | |||
| 1970 Dec 12 | 0830 | 89.12 160 x 301 x 65.5 | |
| 1970 Dec 13 | 0221 | 89.23 163 x 309 x 65.4 | |
| Orbit raise | |||
| 1970 Dec 14 | 0230 | 89.53 181 x 323 x 65.42 (RAE) | |
| 1970 Dec 15 | 2129 | 89.47 163 x 332 x 65.4 | |
| 1970 Dec 16 | 0220? | Engine sep | |
| 0622? | Retrofire | ||
| 0632? | PO sep | ||
| 0636? | Entry | ||
| 0652? | Landed | ||
1988-093A
| Kosmos-1975 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Oct 11 | 0801:00 | Launch by 11K68 | Plesetsk 41.13E |
| T+2:00 St 1 sep | |||
| T+3:33? GO sep | |||
| T+4:38? St 2 sep | |||
| T+5:20? S5M burn 1 | |||
| 0807 | T+6:48 S5M MECO1 km | 60? x 650 x 82.5 | |
| T+40:58? S5M burn 2 | |||
| T+41:08? S5M MECO2 | |||
| 0842? | T+41:38? S5M sep | ||
| 1988 Oct 11 | 97.69 632x664x82.5 | ||
1977-115A
Zenit-2M; carried a capsule, possibly the 26KS type.
| Kosmos-966 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1977 Dec 12 | 0940 | Launch by Soyuz-U | Baikonur |
| 0944 | Blok-I burn | ||
| 0948 | Blok-I sep | ||
| 1977 Dec 12 | 89.50 203 x 295 x 65.0 | ||
| 1977 Dec 22 | Capsule sep | ||
| 1977 Dec 23 | 89.36 199 x 285 x 65.0 | ||
| 1977 Dec 24 | |||
| 0610? | Deorbit | ||
| 0620? | PO sep | ||
| 0626? | Entry | ||
| 0640? | Landed | ||
1973-005A
In Jan 1973 the 11K65M rocket was launched for the first time from the GTsP4 range at Kapustin Yar near Volgograd. It orbited a Tsiklon navsat with a demonstration payload.
| Kosmos-546 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1973 Jan 26 | 1144:45 | Launch by 11K65M | GTsP4 |
| 1146? | Stage 2 burn | ||
| 1152? | Stage 2 coast | ||
| 1217? | Stage 2 burn 2 | ||
| 1218? | Stage 2 sep | ||
| 1973 Jan 29 | 1430 | 96.51 575 x 614 x 50.66 (RAE) | |
1961-001B
SAMOS 2 (Agena 2102), in January 1961, was one of the few successful missions, but its photos were disappointing. Orbit mass of SAMOS and Agena totalled 1915 kg. SAMOS 2 was part of the Program 101 series. The third Program 101 satellite, Agena 2103, was used mainly for engine static firings.
The satellite was another combined E-1/F-1 payload. The E-1 payload was mounted underneath F-1 and had a small field of view while F-1 obstructed it. F-1 was ejected to improve the field of view: this may have caused loss of contact with the vehicle.
| SAMOS 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1961 Jan 31 | 2021:19 | Launch by Atlas Agena A | NMFPA |
| 2023:42 | BECO (T+2:23) | ||
| 2025:18 | SECO (T+3:59) | ||
| 2025:37 | VECO (T+4:18) | ||
| 2025:39 | Atlas sep (T+4:20) | ||
| T+4:35 Nose cone ejected | |||
| T+4:35 Horizon scanner fairings ejected | |||
| 2029:36 | Agena burn (T+8:17) | ||
| 2031:33 | Agena MECO (T+10:14) | 480 x 576 x ? (VCR) | |
| 1961 Feb 2? | Ferret payload ejected on orbit 21 | ||
| End of transmissions | |||
| 1961 Feb 2 | 94.91 474 x 554 x 97.4 | ||
| 1961 Mar 28 | 94.89 474 x 552 x 97.4 | ||
| 1967 Apr 5 | 94.53 463 x 528 x 97.3 | ||
| 1971 Dec 15 | 92.62 386 x 418 x 97.2 | ||
| 1973 Jun 28 | 90.62 298 x 311 x 97.2 | ||
| 1973 Oct 21 | Reentered | ||
1965-007A
The S-017 payload, OSO B, was damaged in an accident on 1964 Apr 14 when the Altair X-248A6 third stage ignited during a ground test and the vehicle launched itself to the building ceiling. Unlike the later X-258, the X-248 igniter was sensitive to electrostatic potentials generated by normal activity in the clean room. There were three fatalities.
Parts from OSO B were combined with an engineering prototype to create OSO B2, which was launched at 1636 on 1965 Feb 3 by a Delta C from Cape Canaveral. 12 minutes later, Orbiting Solar Observatory 2 was in a 96.40 min, 550 x 634 km x 32.9 deg orbit. It transmitted regularly until 1965 Nov and was used occasionally until mid 1966.
| OSO 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1965 Feb 3 | 1636:00 | Launch by Delta 29 | CK LC17B |
| 1638:26 | T+2:26 MECO | ||
| Thor 411 sep | |||
| 1638 | Delta S/N 20110 burn, 2:26 | ||
| 1639:03 | T+3:03 Fairing | ||
| 1641 | Delta SECO | ||
| T+11:22 spinup | |||
| 1647:24 | T+11:24 St 2 sep | ||
| 1647:28 | T+11:28 Altair burn 23s | ||
| 1647:50 | T+11:50 Altair burnout | ||
| T+12:52 Arms deployed | |||
| 1649:28 | T+13:28 Altair sep | 96.40 550 x 634 x 32.9 | |
| 1965 Nov 6 | Gas depleted, end of main mission; turned off | ||
| 1966 Jun 1 | Reactivate for end-of-life tests | ||
| 1966 Jun 6 | End of operations | ||
| 1989 Aug 9 | Reentered | 146 x 148 x 32.8 | |
1989-079A
RCS was 29m2; no debris tracked.
| Kosmos-2046 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Sep 27 | 1620:00 | Launch by Tsiklon I from Baykonur | |
| 1622 | Stage 1 sep | ||
| 1624 | Stage 2 sep | ||
| 1708 | AKM burn | ||
| 1989 Oct 4 | 92.79 405x416x65.0 | ||
| 1991 Apr 11.1 | 91.39 269x415x65.0 from 92.77 402x417x65.0 | ||
| 1991 Apr 11.2 | 90.95 227x414x65.0 | ||
| 1991 Apr 12.2 | 89.38 213x274x65.0 | ||
| 1991 Apr 13.7 | 89.13 204x257x65.0 | ||
| 1991 Apr 16.0 | 88.40 176x214x65.0 | ||
1985-090A
The Resurs-O1 No. 1L satellite (11F697 No. 1L) was launched on 1985 Oct 3 into an 0930LT sun-synch orbit and named Kosmos-1689.
| Kosmos-1689 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 Oct 3 | 0548 | Launch by Vostok 8A92M | KB |
| 0553? | Blok E burn | ||
| 0558? | Blok E MECO | ||
| 1985 Oct 3 | 572x657x98.0 | ||
| 1988 Dec 25 | end of ops | ||
1976-128A
| Kosmos-887 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1976 Dec 28 | 0750 | Launch by 11K65M | Plesetsk |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| T+2:12 St 2 burn 59km | |||
| T+2:27 Fairing sep 76km | |||
| 0758? | 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 | |||
| 0853? | T+1:02:50 St 2 sep | ||
| 1976 Dec 28 | 104.8 954x1018x82.9 | ||
1977-092A
The second Ekran (Ekran No. 12L) was launched on 1977 Sep 20 by Proton-K from Baykonur. The spacecraft was stationed at 99E but on 1978 Jun 23 its nickel-hydrogen battery exploded, distributing numerous fragments in the geostationary ring. The spacecraft was able to operate through 1980 via its solar panels and backup battery.
| Ekran No. 12L | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1977 Sep 20 | 1728 | Launch by Proton-K | KB |
| 1737 | Stage 3 sep | ||
| 1845? | DM burn 1 | ||
| 1977 Sep 21 | 0001? | DM burn 2 | |
| 0005? | DM sep | ||
| 1977 Sep 21 | 1426.66 35580 x 35622 x 0.4 GEO 92.2E+2.4E | ||
| 1977 Sep 28 | 1435.99 35766 x 35802 x 0.4 GEO 98.7E | ||
| 1977 Dec 24 | 1435.93 35696 x 35870 x 0.2 GEO 99.0E | ||
| 1978 Jun 23 | NH2 battery explosion | ||
| 1978 Jul 8 | 1436.24 35744 x 35834 x 0.2 GEO 98.8E | ||
| 1978 Oct 3 | 1436.53 35678 x 35911 x 0.3 GEO 95.6E+0.1W | ||
| 1979 Jan | 1436.9 | ||
| 1979 Jun | GEO 54E | ||
| 1979 Jul | GEO 2W | ||
| 1980 Jul 6 | GEO | ||
| 1982 Dec 29 | 1436.44 35664 x 35922 x 3.6 GEO 97.2E+0.09W | ||
| 1985 Feb 6 | 1436.84 35653 x 35948 x 11.3 GEO 66.9E+0.2W | ||
1978-009A
Molniya-3 F9 was launched in Jan 1978 to the B plane.
| Molniya-3 No. 20 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1978 Jan 24 | 0651 | Launch by 8K78M | PL |
| BVGD sep | |||
| GO sep | |||
| T+4:46 Blok A sep | |||
| T+4:56 KhO sep | |||
| T+8:46 Blok-I MECO | |||
| 0659 | T+8:50 Blok-I sep | ||
| T+53:16 BOZ burn | |||
| 0744 | T+53:56 BOZ sep | ||
| ML burn | |||
| T+56:46 ML MECO | |||
| 0747 | T+56:54 ML sep | ||
| 736.3 646 x 40618 x 62.8 | |||
| 1978 Jan | 718.0 652 x 39718 x 62.8 | ||
| 1980 Nov 2 | end of ops | ||
| 1990 Apr 24 | reentered | ||
1984-103A
Two-tone telemetry; Medium res satellite
| Kosmos-1600 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1984 Sep 27 | 0810 | Launch by Soyuz | KB |
| 0814 | Blok I burn | ||
| 0818 | Blok I MECO | ||
| 0819 | Blok I sep | ||
| 1984 Sep 27 | 205 x 381 x 70.0 | ||
| 2120? | Orbit raise | ||
| 1984 Sep 28 | 350x417x70.0 | ||
| 1984 Oct 8 | 352x417x70.0 | ||
| 1984 Oct 11 | |||
| 1309? | Deorbit | ||
| 1318? | PO sep | ||
| 1335? | Entry | ||
| 1352? | Landed | ||
1966-078A
Luna-11 was a modified lunar satellite, designated E-6LF No. 101. The E-6LF probes were larger than Luna-10 and the instrument section did not separate from the DU. It was intended for lunar photography, but the attitude control failed after orbit insertion and the images were of deep space instead of the Moon.
| Luna-11 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Aug 24 | 0803 | Launch by Molniya | KB |
| 0808 | Blok-A sep | ||
| 0808 | Blok-I burn | ||
| 0812 | Blok-I sep | ||
| 0903? | BOZ burn | ||
| 0904? | Blok-L burn | ||
| 0907? | Blok-L sep | ||
| 1966 Aug 26 | 1902 | TCM | |
| 1966 Aug 27 | 2145? | Modules sep | |
| 1966 Aug 27 | 2149 | LOI | |
| 1966 Aug 27 | Lunar orbit | 129 x 1230 x 9.7 | |
| 1966 Oct 1 | 0203 | End of tx | |
1988-049A
| Kosmos-1952 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Jun 11 | 1000:00 | Launch by Soyuz | KB |
| 1004 | Blok-I burn | ||
| 1008 | Blok-I sep | ||
| 1988 Jun 11 | 89.3 206x272x70.0 | ||
| 1988 Jun 12 | 89.68 230 x 286 x 70.0 | ||
| 1988 Jun 23 | 89.60 227 x 281 x 70.0 | ||
| 1988 Jun 25 | |||
| 0656? | Deorbit | ||
| 0706? | PO sep | ||
| 0712? | Entry | -179 x 258 | |
| 0728? | Landed | ||
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