Tuesday, December 31, 1991
Sunday, December 29, 1991
Progress M-3
1990-020A
Progress M 11F615A55 No. 203 (7K-TGM No. 203) was launched on 1990 Feb 28 as Progress M-3.
| Progress M-3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Feb 28 | 2310:57 | Launch by Soyuz | KB |
| 2315 | Blok-I burn | ||
| 2319 | Blok-I sep | ||
| 1990 Mar 1 | 0000 | 88.51 183 x 218 x 51.6 | |
| 0230 | 88.60 183 x 227 x 51.6 | ||
| 0700 | 90.60 276 x 331 x 51.6 | ||
| 1990 Mar 2 | 0230 | 90.63 280 x 330 x 51.6 | |
| 2130 | 91.22 321 x 347 x 51.6 | ||
| 1990 Mar 3 | 0104:32 | Docked with Mir KDP2 | |
| 1990 Mar 4 | 0230 | 92.36 378 x 402 x 51.6 | |
| 1990 Apr 23 | TCM | ||
| 1990 Apr 26 | 2024:43 | Undocked | |
| 1990 Apr 28 | 0052 | Reentered | |
Kosmos 410
1971-040A
Kosmos-410 was launched in May 1971 from Baikonur. The Gektor satellite carried a Nauka package with an electron detector.
| Kosmos-410 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 May 6 | 0620:01 | Launch by 11A57 | KB |
| 0624 | Blok-I burn | ||
| 0628 | Blok-I sep | ||
| 1971 May 7 | 0900 | 89.34 204 x 278 x 65.0 | |
| 1971 May 12 | 0155 | 89.23 201 x 272 x 65.0 | |
| 1971 May 16 | 1257 | 89.15 197 x 266 x 65.0 | |
| 1971 May 17 | Nauka sep | ||
| 1971 May 18 | 0343? | Retrofire | |
| 0353? | PO sep | ||
| 0359? | Entry | ||
| 0415? | Landed after 11.90d | ||
Kosmos 228
1968-053A
The second Gektor launch went to a 51.6 degree orbit in the summer of 1968. It carried a supplementary radiation studies package on its 12 day flight.
| Kosmos-228 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1968 Jun 21 | 1200:03 | Launch by 11A57 | KB |
| 1204 | Blok-I burn | ||
| 1209 | Blok-I sep | ||
| 1968 Jun 21 | 1446 | 88.79 204 x 225 x 51.6 | |
| 1968 Jun 22 | 1200 | 89.00 199 x 252 x 51.62 (RAE) | |
| 1968 Jun 29 | 1056 | 88.87 200 x 236 x 51.6 | |
| 1968 Jul 1 | 0700? | Nauka capsule sep | |
| 1968 Jul 2 | 1721 | 88.79 199 x 299 x 51.6 | |
| 1968 Jul 3 | 0944? | Deorbit | |
| 1004? | Landed after 11.92d | ||
Sunday, December 22, 1991
Kosmos 1894
1987-091A
Kosmos-1984,launched in Oct 1987,was an Oko-S satellite stationed at 24W.
| Kosmos-1894 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 Oct 28 | 1515:00 | Launch by Proton | KB |
| 1524 | Stage 3 sep | ||
| 1630? | DM burn 1 | ||
| 2335? | DM burn 2 | ||
| 2355? | DM sep | ||
| 1987 Oct 29 | 1441.76 35834 x 35960 x 1.3 GEO 88.8E+1.4W | ||
| 1987 Dec 2 | 1449.42 35915 x 36178 x 1.2 GEO 16.4W+3.3W | ||
| 1987 Dec 7 | mv in | 1436.04 35752 x 35818 x 1.2 GEO 25.0W | |
| 1987 Dec 22 | 1436.01 35777 x 35792 x 1.1 GEO 23.4W | ||
| 1988 Dec 5 | 1436.12 35770 x 35803 x 0.2 GEO 23.8W | ||
| 1989 Jul 7 | 1436.18 35784 x 35792 x 0.3 GEO 23.7W | ||
| 1990 Jun 12 | 1436.09 35776 x 35796 x 1.2 GEO 24.0W | ||
| 1991 May 24 | 1436.08 35771 x 35801 x 2.1 GEO 24.0W | ||
Thursday, December 19, 1991
Wednesday, December 18, 1991
Kosmos 601
1973-075A
Kosmos-601 (DS-P1-Yu No. 60) was a DS-P1-Yu satellite launched from Plesetsk in Oct 1973. It was placed in a subgroup 2 orbit with an apogee of 1531 km.
| Kosmos-601 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1973 Oct 16 | 1400 | Launch by 11K63 | PL |
| 1402 | Stage 2 burn | ||
| 1407? | Stage 2 sep | ||
| 1973 Oct 18 | 1200 | 102.28 200 x 1531 x 81.9 (RAE) | |
| 1974 Feb | End of ops | ||
| 1974 Aug 15 | Reentered | ||
Sunday, December 15, 1991
Kosmos 47
1964-062A
The first Voskhod class spacecraft to fly was 3KV No. 2, launched on a test flight under the cover name Kosmos-47 in Oct 1964. It carried two instrumented mannequins. The spacecraft was recovered after one day in orbit.
| Kosmos-47 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1964 Oct 6 | 0700:00 | Launch by 11A57 | KB |
| 0704 | Blok-I burn | ||
| 0709 | Blok-I MECO | ||
| 90.07 174 x 383 x 64.6 | |||
| 1964 Oct 7 | 0710? | Retrofire | |
| 0730:00 | Landed after 1.0d | ||
Tuesday, December 3, 1991
Kosmos 1653
1985-038A
The 17F41 No. 52 (Resurs F-1) spacecraft was launched in May 1985 and named Kosmos-1653.
| Kosmos-1653 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 May 22 | 0835 | Launch by Soyuz-U | PL LC41 |
| 0843 | Blok-I sep | 210 x 295 x 82.3 | |
| 1985 May 23 | 273 x 295 x 82.3 | ||
| 1985 May 27 | 268 x 275 x 82.3 | ||
| 1985 Jun 2 | 269 x 274 x 82.3 | ||
| 1985 Jun 7 | |||
| 0500? | Deorbit | ||
| 0510? | PO sep | ||
| 0520? | Entry | ||
| 0532? | Landed | ||
Monday, December 2, 1991
MOS-1
1987-018A
NASDA's Marine Observation Satellite, MOS-1, carried radiometers to measure ocean conditions. The satellite was named Momo (Peach or Peach Blossom) once on orbit. It was built by Nippon Electric.
| Momo | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 Feb 19 | 0123 | Launch by N-2 | TNSC |
| T+0:39 SOB 7-9 on | |||
| T+0:40 SOB 1-6 off | |||
| T+1:19 SOB 7-9 off | |||
| T+1:25 SOB 1-9 sep, 22 km alt | |||
| T+4:31 St 1 MECO | |||
| T+4:37 VECO | |||
| T+4:39 Stage 1 sep at 155 km | |||
| T+4:45 SES-1 at 163 km 384s | |||
| 0128 | T+4:53 Fairing | ||
| 0134 | T+11:09 SECO-1 411 km | 366? x 910 x 99.1 | |
| 0213 | T+50:58 SES-2 8s 221m/s? | ||
| 0214 | T+51:06 SECO-2 | ||
| 0215 | T+52:54 MOS/Stage 2 sep | 103.33 911 x 912 x 99.1 | |
| 0220 | T+57:54 SES-3 3s | ||
| 0220 | T+57:57 SECO-3 | ||
| 0223 | T+1:00:27 SES-4 17s | ||
| 0223 | T+1:00:44 SECO-4 | 100.24 636 x 903 x 97.5 | |
| 1987 Feb | OTM | ||
| 1987 Jun | Begin operational phase | ||
| 1987 Jul | OTM | ||
| 1987 Jul 28 | Safemode, attitude anomaly | ||
| 1987 Dec | OTM | ||
| 1988 Apr | OTM | ||
Friday, November 29, 1991
Tuesday, November 26, 1991
Monday, November 25, 1991
Molniya 330
1986-079A
Molniya-3 F32 (N30) was launched into the E plane in Oct 1986.
| Molniya-3 No. 41 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1986 Oct 20 | 0849 | 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 | |||
| 0857 | T+8:50 Blok-I sep | ||
| T+53:16 BOZ burn | |||
| 0942 | T+53:56 BOZ sep | ||
| ML burn | |||
| T+56:46 ML MECO | |||
| 0945 | T+56:54 ML sep | ||
| 1986 Oct 20 | 82.82 207 x 618 x 62.8 | ||
| 699.35 621 x 38820 x 62.9 (D) | |||
| 698.7 602 x 38805 x 62.9 | |||
| 2130 | 702.4 626 x 38977 x 62.9 | ||
| 1986 Oct 26 | 717.0 627 x 39692 x 62.9 | ||
| 1986 Oct 30 | 717.7 625 x 39724 x 62.9 | ||
Sunday, November 24, 1991
Kosmos 756
1975-076A
| Kosmos-756 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1975 Aug 22 | 0211? | Launch by 8A92M | Plesetsk |
| 0216? | Blok E burn | ||
| 0221? | Blok E sep | ||
| 1975 Aug 22 | 97.3 622x634x81.2 | ||
| 1992 Nov 5 | reentered | ||
Saturday, November 23, 1991
Sunday, November 17, 1991
Kosmos 1788
1986-083A
| Kosmos-1788 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1986 Oct 27 | 1240:00 | Launch by 11K65M | Plesetsk 41.7E |
| 1300? | Stage 2 sep | ||
| 1986 Oct 27 | 462x516x65.83 | ||
| 1991 Jun 21 | reentered | ||
Friday, November 15, 1991
Friday, November 8, 1991
Kosmos 298
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? | ||
Tuesday, November 5, 1991
Kosmos 383
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 | ||
Monday, November 4, 1991
Kosmos 1975
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 | ||
Tuesday, October 29, 1991
Kosmos 546
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) | |
Monday, October 28, 1991
Wednesday, October 23, 1991
Wednesday, October 16, 1991
OSO 2
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 | |
Payload:
- Sail:
- Solar UV spectrometer 300-1400A, HCO
- Solar X monitor 2-20A,44-60A (0.6-6 keV,0.2-0.28 keV), NRL
- UV telescope, NRL (1216, 388 and 304 A).
- White light coronagraph, NRL
- Wheel:
- Zodiacal light photometers 4750-8000A, Minnesota
- Low energy Gamma-ray detector 0.1-0.7 MeV, GSFC
- High energy Gamma ray solar and extrasolar: 0.1-1 GeV, New Mexico
- Astronomical UV spectrophotometer, 900-2000 and 1800-3800A, GSFC
Saturday, October 12, 1991
Kosmos 2046
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 | ||
Tuesday, October 8, 1991
Kosmos 1689
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 | ||
Sunday, September 29, 1991
Ekran 2
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 | ||
Thursday, September 26, 1991
Molniya 309
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 | ||
Friday, September 20, 1991
Kosmos 1600
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 | ||
Luna 11
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 | |
Kosmos 1952
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 | ||
Wednesday, September 18, 1991
Tuesday, September 17, 1991
Explorer 18
1963-046A
IMP A (Interplanetary Monitoring Platform A, or Interplanetary Monitoring Platform 1 after launch) was the first in the series. The old NASA designation was S-74; the flight spacecraft was S/N 02.
Launch was 1963 Nov 27, 0230:01 by Delta C from Canaveral LC17B. Orbit insertion was at 0236:07 into a 192 x 197616 km x 33.3 deg orbit; the planned apogee was 277000 km but the Altair stage underburned. IMP I operated until 1965 Mar 25. The satellite was also called Explorer 18.
| IMP 1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1963 Nov 27 | 0230:01 | Launch by Delta C | CC LC17B |
| 0232:27 | T+2:26 Thor MECO | ||
| T+2:28 Delta S/N 20012 SES, 2:51 | |||
| T+3:02 Fairing | |||
| 0235:23 | T+5:17s Delta SECO | ||
| 0235:37 | T+5:40s Delta sep | -640? x 192 x 33.3 | |
| 0235:43 | T+5:44s Altair 2 RH-60 burn, 24s | ||
| 0236:08 | T+6:07 Altair 2 burnout | ||
| 0301:21 | T+31:20 Altair sep | 192 x 197616 x 33.3 | |
| 0301:21 | IMP magnetometer deployed | ||
| 2112? | Pass EL1:4 | ||
| 1964 Apr 3 | 5599.52 2072 x 194079 x 35.3 | ||
| 1964 Sep 4 | 5602.27 3864 x 192355 x 36.4 | ||
| 1965 Mar 25 | 5610.65 4385 x 192043 x 35.2 | ||
| 1965 Mar 25 | End of ops | ||
Monday, September 16, 1991
Kosmos 176
1967-086A
DS-P1-Yu No. 10 was the second DS-P1-Yu satellite in the high apogee polar Subgroup 2.
| Kosmos-176 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1967 Sep 12 | 1700 | Launch by 11K63 | PL |
| 1702 | Stage 2 burn | ||
| 1707? | Stage 2 sep | 102.2 196 x 1525 x 81.9 | |
| 1967 Nov 11 | end of ops | ||
| 1968 Mar 3 | Reentered | ||
Kosmos 2035
1989-060A
| Kosmos-2035 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Aug 2 | 1129:59 | Launch by Soyuz | PL |
| 1134 | Blok-I burn | ||
| 1138 | Blok-I sep | ||
| 1989 Aug 2 | 88.52 164 x 237 x 82.6 | ||
| 1989 Aug 3 | 88.70 179 x 239 x 82.6 | ||
| 1989 Aug 8 | 90.39 230 x 356 x 82.6 | ||
| 1989 Aug 11 | 90.33 229 x 351 x 82.6 | ||
| 1989 Aug 12 | 89.22 229 x 242 x 82.6 | ||
| 1989 Aug 15 | 89.16 227 x 238 x 82.6 | ||
| 1989 Aug 16 | |||
| 0807? | Deorbit | ||
| 0817? | PO sep | ||
| 0824? | Entry | -196 x 231 | |
| 0840? | Landing | ||
Saturday, September 14, 1991
Thursday, September 12, 1991
Kosmos 1969
1988-084A
| Kosmos-1969 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Sep 15 | 1500:00 | Launch by Soyuz | PL |
| 1509 | Blok I sep | ||
| 1988 Sep 15.9 | 89.64 167x347x67.1 | ||
| 1988 Sep 22 | Orbit raise | 89.78 178x349x67.1 from 89.11 159x302 | |
| 1988 Sep 28 | 89.28 169 x 308 x 67.1 | ||
| 1988 Sep 30 | Orbit raise | 89.83 179x353x67.1 from 89.17 167x300 | |
| 1988 Oct 6 | Fid. SpK-1 | ||
| 1988 Oct 11 | Orbit raise | 89.84 183x350x67.1 from 88.93 163x281 | |
| 1988 Oct 21 | Orbit lower | 88.67 157 x 259 | |
| 1988 Oct 23 | Orbit raise | 89.83 186x346x67.1 from 88.43 153x241 | |
| 1988 Oct 30 | Fid. SpK-2 | ||
| 1988 Nov 3 | Orbit raise | 89.69 179x340x67.1 from 88.96 173x273 | |
| 1988 Nov 9 | Orbit raise | 89.61 170x341x67.1 from 89.03 168x286 | |
| 1988 Nov 12 | 89.32 165x316x67.1 | ||
| 1988 Nov 17 | 0344? | reentered | |
Friday, September 6, 1991
Soyuz TM-7
1988-104A
7K-STM spaceship 11F732 No. 57 (Soyuz TM-7) was launched on 1988 Nov 26, commanded by Aleksandr Volkov and carrying flight engineer Sergey Krikalyov and French astronaut-researcher Gen. Jean-Loup Chretien. The mission was code-named Aragats. Soyuz TM-7 docked with the rear Kvant port of the Mir complex on Nov 28.
On Dec 22, Volkov, Krikalyov, and station doctor Polyakov entered the Soyuz TM-7 and moved it to the front port.
- Komandir Aleksandr Volkov, VVS
- Bortinzhener Sergey Krikalyov, NPO Energiya
- Kosmonavt-issledovatel' Gen. Jean-Loup Chretien, AAF, CNES
Crew
| Soyuz TM-7, Flight 1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Nov 26 | 1549 | Launch by Soyuz-U2 | KB |
| 1551 | Blok-BVGD sep, T+1:58 | ||
| 1553 | Blok-A sep, T+4:48 | ||
| 1557 | Blok-I cutoff | ||
| 1558 | Blok-I sep | ||
| 1700 | 88.79 194 x 235 x 51.6 | ||
| 193 x 234 x 51.6 | |||
| 2130 | 89.96 253 x 292 x 51.6 | ||
| 1988 Nov 27 | 89.93 252 x 291 x 51.6 | ||
| 1900 | 89.98 256 x 291 x 51.6 | ||
| 1988 Nov 28 | 1716 | Docked with 37KE +X | |
| 89.96 253 x 292 x 51.62 | |||
| 1988 Nov 29 | 91.60 337 x 370 x 51.6 | ||
| 1988 Nov 30 | 91.60 337 x 369 x 51.6 | ||
- Komandir Aleksandr Volkov, VVS
- Bortinzhener Sergey Krikalyov, NPO Energiya
- Vrach-issledovatel' Dr. Valeriy Polyakov, IMBP
Crew
| Soyuz TM-7, Flight 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Dec 22 | 0520 | Crew entry, hatch closed | |
| 0645 | Undocked 37KE +X | ||
| 0659 | Docked Mir -X | ||
| 1988 Dec 24 | 327 x 355 x 51.6 | ||
| Soyuz TM-7, Flight 3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Apr 25 | 2130 | 92.74 401 x 417 x 51.5 | |
| 1989 Apr 26 | 2328 | Undocked -X | |
| 1989 Apr 27 | 0203? | Deorbit | |
| 0207? | DO CO | ||
| 0231? | Module sep | ||
| 0235? | Entry | ||
| 0257:58 | Landed | ||
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