Encyclopedia Astronautica
Plesetsk LC32/2


Tsiklon launch complex. Construction of this highly-automated launch complex for the Tsiklon-3 launch vehicle started in 1970. The complex was designed by the Transmash Design bureau led by Chief Designer V N Solovyev. The complex consisted of two pads. The vehicle was assembled and integrated with its payload in the assembly building. It was then delivered to the launch pad by railway in a horizontal position. A launch pad erector placed the rocket into vertical position. No service tower was needed for the storable-propellant booster.

Longitude: 40.7895 deg.
Latitude: 62.9057 deg.
First Launch: 1977.06.24.
Last Launch: 2004.12.24.
Number: 27 .

More... - Chronology...


Associated Spacecraft
  • Tselina-D Ukrainian military naval signals reconnaisance satellite. 77 launches, 1970.12.18 (Cosmos 389) to 1994.05.25 (Tselina-D). The Tselina D was the detailed observation portion of the two-satellite Tselina ELINT satellite system. More...
  • Meteor-2 Russian earth weather satellite. 22 launches, 1975.07.11 (Meteor 2-01) to 1993.08.31 (Meteor 2-21). Successor to the Meteor-1 weather satellite. The Meteor-2 had a longer design operational life (one year vs. More...
  • AUOS Ukrainian technology satellite. 14 launches, 1976.06.19 (Intercosmos 15) to 2009.01.30 (Koronas-F). Standardized bus for low earth orbit scientific studies and testing of new systems and components of satellite under space flight conditions. More...
  • Magion Czech earth magnetosphere satellite. 5 launches, 1978.10.24 (Magion 1) to 1996.08.29 (Magion 5). The Czechoslovak satellite MAGION researched the magnetosphere and ionosphere of the earth. More...
  • Radio Russian amateur radio communications satellite. 9 launches, 1978.10.26 (Radio Sputnik 1) to 1994.12.26 (Radio-ROSTO RS-15). More...
  • Okean-E Ukrainian earth resources radar satellite. 2 launches, 1979.02.12 (Cosmos 1076) to 1980.01.23 (Cosmos 1151). First prototype of Okean series. Development of methods for obtaining operational information on the Pacific Ocean. More...
  • Geo-IK Russian earth geodetic satellite. 14 launches, 1981.01.23 (Geo-IK no. 1) to 1994.11.29 (Geo-IK). Development of a second generation geodetic satellite system began in 1977. More...
  • Okean-OE Ukrainian earth resources radar satellite. 2 launches, 1983.09.28 (Cosmos 1500) to 1984.09.28 (Cosmos 1602). More...
  • Strela-3 Russian military store-dump communications satellite. Operational, first launch 1985.01.15. Said to have initially been developed for the GRU. More...
  • Okean-O1 Ukrainian earth resources radar satellite. 9 launches, 1986.07.28 (Cosmos 1766) to 2004.12.24 (Sich-1M). Third generation Soviet oceanographic research satellite, equipped with a side-looking radar, radiometer, and multi-spectral scanner. More...
  • Taifun-3 Russian military target satellite. 2 launches, 1988.12.23 (Cosmos 1985) to 1989.12.27 (Cosmos 2053). Specifications for a third generation Taifun-3 system were developed in 1980 with flight trials to have started in 1984. More...
  • MS-1 Ukrainian earth land resources satellite. 2 launches, 2004.12.24 (Mikron) to 2007.04.17 (MisrSat 1). Ukrainian microsatellite bus that could be equipped with imaging or other scientific or technical equipment. More...

Associated Launch Vehicles
  • Tsiklon-3 Ukrainian orbital launch vehicle. The Tsyklon 3 was developed in 1970-1977 as a part of a program to reduce the number of Soviet booster types. The first two stages were derived from the 8K68 version of the R-36 ICBM, while the restartable third stage was derived from that of the R-36-O. Compared to the Tsyklon 2, the launch vehicle increased payload to 4 metric tons, provided for completely automated launch operations, and had increased orbital injection accuracy. More...

Associated Launch Sites
  • Plesetsk Plesetsk was the Soviet Union's northern cosmodrome, used for polar orbit launches of mainly military satellites, and was at one time the busiest launch centre in the world. The collapse of the Soviet Union put the main launch site of Baikonur in Kazakh territory. It now seems that once the Proton rocket is retired, Baikonur will be abandoned and Plesetsk will be Russia's primary launch centre. Upgrades to existing launch facilities will allow advanced versions of the Soyuz rocket and the new Angara launch vehicle to be launched from Plesetsk. Plesetsk's major drawback was the lower net payload in geosynchronous orbit from a northern latitude launch site. However Russia is planning to remove the disadvantage by looping geosynchronous satellites around the moon, using lunar gravity to make the necessary orbital plane change. More...

Plesetsk LC32/2 Chronology


1977 June 24 - . 10:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. LV Configuration: Tsiklon-3 No. 2L.
  • Cosmos 921 - . Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 10095 . COSPAR: 1977-055A. Apogee: 651 km (404 mi). Perigee: 587 km (364 mi). Inclination: 75.8000 deg. Period: 97.10 min. Summary: Launch vehicle test. Dummy payload. Investigation of the upper atmosphere and outer space..

1977 September 24 - . 10:15 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. FAILURE: Probable failure of launch vehicle stage to reach proper orbit.. Failed Stage: 3.
  • Cosmos 956 - . Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. Decay Date: 1982-06-27 . USAF Sat Cat: 10375 . COSPAR: 1977-095A. Apogee: 864 km (536 mi). Perigee: 355 km (220 mi). Inclination: 75.8000 deg. Period: 96.80 min. Summary: Launch vehicle test. Dummy payload. Probable failure of launch vehicle stage to reach proper orbit. Investigation of the upper atmosphere and outer space..

1977 December 27 - . 08:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. FAILURE: Probable failure of launch vehicle stage to reach proper orbit.. Failed Stage: 3.
  • Cosmos 972 - . Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 10539 . COSPAR: 1977-123A. Apogee: 1,157 km (718 mi). Perigee: 712 km (442 mi). Inclination: 75.8000 deg. Period: 103.70 min. Summary: Launch vehicle test. Dummy payload. Probable failure of launch vehicle stage to reach proper orbit. Investigation of the upper atmosphere and outer space..

1978 June 28 - . 17:35 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1025 - . Payload: Tselina-D Mass model no. 16. Mass: 4,375 kg (9,645 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. Decay Date: 2007-03-10 . USAF Sat Cat: 10973 . COSPAR: 1978-067A. Apogee: 567 km (352 mi). Perigee: 551 km (342 mi). Inclination: 82.5000 deg. Period: 95.80 min.

1978 October 26 - . 07:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1045 - . Payload: Meteor-2 Mass Model. Mass: 2,670 kg (5,880 lb). Nation: USSR. Agency: MO. Class: Earth. Type: Weather satellite. Spacecraft: Meteor-2. USAF Sat Cat: 11084 . COSPAR: 1978-100A. Apogee: 1,705 km (1,059 mi). Perigee: 1,686 km (1,047 mi). Inclination: 82.5000 deg. Period: 120.30 min. Summary: Probable oceanographic. Investigation of the upper atmosphere and outer space. .
  • Radio-2; Radio Sputnik 2 - . Payload: RS-2. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Radio. USAF Sat Cat: 11086 . COSPAR: 1978-100C. Apogee: 1,705 km (1,059 mi). Perigee: 1,686 km (1,047 mi). Inclination: 82.6000 deg. Period: 120.30 min. Summary: Launched with Cosmos-1045. Amateur radiocommunication and scientific and technical experiments and study projects by students at higher educational establishments..
  • Radio Sputnik 1 - . Payload: RS-1. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Radio. USAF Sat Cat: 11085 . COSPAR: 1978-100B. Apogee: 1,707 km (1,060 mi). Perigee: 1,686 km (1,047 mi). Inclination: 82.6000 deg. Period: 120.40 min. Summary: Launched with Cosmos-1045. Amateur radiocommunication and scientific and technical experiments and study projects by students at higher educational establishments..

1979 February 12 - . 13:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1076 - . Payload: Okean-E no. 1. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: MO. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-E. Completed Operations Date: 1980-03-13 . Decay Date: 2001-08-10 . USAF Sat Cat: 11266 . COSPAR: 1979-011A. Apogee: 530 km (320 mi). Perigee: 514 km (319 mi). Inclination: 82.5000 deg. Period: 95.10 min. Summary: Test mission of Okean satellite without the radar. Development of methods for obtaining operational information on the Pacific Ocean..

1983 November 24 - . 12:33 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1510 - . Payload: Geo-IK no. 4. Mass: 1,500 kg (3,300 lb). Nation: USSR. Agency: MO. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 14521 . COSPAR: 1983-115A. Apogee: 1,524 km (946 mi). Perigee: 1,480 km (910 mi). Inclination: 73.6000 deg. Period: 116.00 min. Summary: Investigation of the upper atmosphere and outer space. .

1984 August 8 - . 12:08 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1589 - . Payload: Geo-IK no. 5. Mass: 1,500 kg (3,300 lb). Nation: USSR. Agency: MO. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 15171 . COSPAR: 1984-084A. Apogee: 1,504 km (934 mi). Perigee: 1,492 km (927 mi). Inclination: 82.6000 deg. Period: 115.90 min. Summary: Investigation of the upper atmosphere and outer space. .

1984 September 28 - . 06:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1602 - . Payload: Okean-OE no. 2. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: MO. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-OE. Completed Operations Date: 1986-12-05 . USAF Sat Cat: 15331 . COSPAR: 1984-105A. Apogee: 628 km (390 mi). Perigee: 597 km (370 mi). Inclination: 82.5000 deg. Period: 97.00 min. Gathering of operational information and continued trials of new kinds of information and measurement apparatus and methods of remote investigation of the seas and oceans and the earth's surface in the interests of science and of various branches of the n ational economy of the USSR.

1986 February 11 - . 06:56 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1732 - . Payload: Geo-IK no. 7. Mass: 1,500 kg (3,300 lb). Nation: USSR. Agency: MO. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 16593 . COSPAR: 1986-015A. Apogee: 1,525 km (947 mi). Perigee: 1,480 km (910 mi). Inclination: 73.6000 deg. Period: 116.00 min. Summary: Investigation of the upper atmosphere and outer space. .

1986 July 28 - . 21:08 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1766 - . Payload: Okean-O1 no. 1. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: MO. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. Completed Operations Date: 1988-10-24 . USAF Sat Cat: 16881 . COSPAR: 1986-055A. Apogee: 631 km (392 mi). Perigee: 601 km (373 mi). Inclination: 82.5000 deg. Period: 97.00 min. Oceanographic. Acquisition of operational oceanographic information in the interests of various branches of the national economy of the USSR and international cooperation; continued trials of new types of informational and measurement apparatus and methods of remote sen sing of the earth's surface and atmosphere.

1987 February 20 - . 04:43 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1823 - . Payload: Geo-IK no. 9. Mass: 1,500 kg (3,300 lb). Nation: USSR. Agency: MO. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. Decay Date: 1987-12-31 . USAF Sat Cat: 17535 . COSPAR: 1987-020A. Apogee: 1,524 km (946 mi). Perigee: 1,479 km (919 mi). Inclination: 73.6000 deg. Period: 116.00 min. Summary: Investigation of the upper atmosphere and outer space. .

1987 July 16 - . 04:25 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1869 - . Payload: Okean-O1 no. 2. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: MO. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. Completed Operations Date: 1989-05-30 . USAF Sat Cat: 18214 . COSPAR: 1987-062A. Apogee: 632 km (392 mi). Perigee: 602 km (374 mi). Inclination: 82.5000 deg. Period: 97.10 min. Summary: Oceanographic. Acquisition of operational oceanographic information in the interests of various branches of the national economy of the USSR and international cooperation. .

1989 June 9 - . 10:10 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. FAILURE: Stage 3 failure - third stage engine did not ignite for second burn.. Failed Stage: 3.
  • Okean - . Payload: Okean-O1 no. 4. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: UNKS. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. COSPAR: F890609A.

1989 August 28 - . 00:14 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 2037 - . Payload: Geo-IK no. 11. Mass: 1,500 kg (3,300 lb). Nation: USSR. Agency: MO. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 20196 . COSPAR: 1989-068A. Apogee: 1,524 km (946 mi). Perigee: 1,485 km (922 mi). Inclination: 73.6000 deg. Period: 116.10 min. Summary: Investigation of outer space. .

1989 September 28 - . 00:04 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Intercosmos 24 - . Payload: AUOS-Z-AV-IK s/n 201. Mass: 1,000 kg (2,200 lb). Nation: USSR. Agency: MOM. Manufacturer: Yuzhnoye. Program: Intercosmos. Class: Technology. Type: Navigation technology satellite. Spacecraft: AUOS. Completed Operations Date: 1995-10-11 . USAF Sat Cat: 20261 . COSPAR: 1989-080A. Apogee: 2,414 km (1,499 mi). Perigee: 499 km (310 mi). Inclination: 82.6000 deg. Period: 115.00 min. US participation; particles and fields experiments; deployed Magion 2. Comprehensive study of the processes of propagation of low-frequency electromagnetic waves in the earth's magnetosphere and their interaction with charged particles of the radiation belts, in cooperation with Bulgaria, Czechoslovakia, the German Democrati c Republic, Hungary, Poland and Romania (the international scientific project entitled 'Aktivny'). Carrying the Czechoslovak Magion-2 satellite.
  • Magion 2 - . Payload: S2-AK. Mass: 50 kg (110 lb). Nation: Czech Republic. Agency: UNKS. Program: Intercosmos. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Magion. USAF Sat Cat: 20281 . COSPAR: 1989-080B. Apogee: 2,441 km (1,516 mi). Perigee: 498 km (309 mi). Inclination: 82.6000 deg. Period: 115.30 min. Deployed from Intercosmos 24 10/3/89; examined signal propogation from Intercosmos 24. Research of the magnetosphere and the ionosphere of the Earth. The Czechoslovak satellite Magion 2 was launched into orbit by the Soviet spacecraft Intercosmos 24. Magion 2 forms a part of the scientific programme of Intercosmos 24 (project Aktivnyj) Exe cution of the scientific programme of the 'Aktivny' project in conjunction with Intercosmos-24, permitting simultaneous spatially separating investigations of plasma processes in circumterrestrial space.

1989 December 27 - . 00:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 2053 - . Mass: 3,000 kg (6,600 lb). Nation: USSR. Agency: MO. Class: Military. Type: Radar calibration target. Spacecraft: Taifun-3. Decay Date: 1997-09-02 . USAF Sat Cat: 20389 . COSPAR: 1989-100A. Apogee: 410 km (250 mi). Perigee: 405 km (251 mi). Inclination: 73.5000 deg. Period: 92.70 min. Believed to be a modernised version of the Taifun-1 satellite, built by NPO Yuzhnoe. The satellite carried 36 small Calibration Spherical Object subsatellites to test Russian radars. These were released between December 27, 1989 and November 1, 1991. While Cosmos 2053 re-entered in 1997, by May 1999 the S5M upper stage was still in a 471 km x 485 km x 73.5 deg orbit. An on-board explosion blew it into 25 new objects.

1990 February 28 - . 00:55 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Okean 2 - . Payload: Okean-O1 no. 5. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: MO. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. Completed Operations Date: 1991-07-18 . USAF Sat Cat: 20510 . COSPAR: 1990-018A. Apogee: 646 km (401 mi). Perigee: 617 km (383 mi). Inclination: 82.5000 deg. Period: 97.40 min. Summary: Oceanographic remote sensing. Gathering of up-to-date oceanographic information and data on ice conditions in the interests of the Soviet economy and international cooperation. .

1991 June 4 - . 08:10 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Okean 3 - . Payload: Okean-O1 no. 6. Mass: 1,950 kg (4,290 lb). Nation: USSR. Agency: MOM. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. Completed Operations Date: 1994-01-04 . USAF Sat Cat: 21397 . COSPAR: 1991-039A. Apogee: 656 km (407 mi). Perigee: 621 km (385 mi). Inclination: 82.5000 deg. Period: 97.50 min. Summary: Oceanography. Gathering of up-to-date oceanographic information and data on ice conditions in the interests of the Soviet economy and international cooperation. Okean 3 ceased working in January of 1994..

1991 December 18 - . 03:54 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Intercosmos 25 - . Payload: AUOS-Z APEKS-IK s/n 301. Mass: 1,000 kg (2,200 lb). Nation: USSR. Agency: MOM. Manufacturer: Yuzhnoye. Program: Intercosmos. Class: Technology. Type: Navigation technology satellite. Spacecraft: AUOS. USAF Sat Cat: 21819 . COSPAR: 1991-086A. Apogee: 2,969 km (1,844 mi). Perigee: 436 km (270 mi). Inclination: 82.6000 deg. Period: 120.50 min. Solar activity monitoring; hosted experiments from Germany, Romania, Bulgaria, Poland, Hungary. Comprehensive study of the effects of artificial impact of modulated electron flows and plasma beams on the ionosphere and magnetosphere of the Earth (forming part of the Apex international scientific project, conducted jointly with Bulgaria, Czechoslovak ia, Germany, Hungary, Poland and Romania.) Launched with the Czechoslovak satellite Magion-3, separated from the space object Intercosmos-25 on 28 Dec 1991, in accordance with the scientific programme of the Apex project.
  • Magion 3 - . Payload: S2-AP. Mass: 52 kg (114 lb). Nation: Czech Republic. Agency: UNKS. Program: Intercosmos. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Magion. USAF Sat Cat: 21835 . COSPAR: 1991-086E. Apogee: 2,943 km (1,828 mi). Perigee: 436 km (270 mi). Inclination: 82.6000 deg. Period: 120.20 min. Separated from Intercosmos 25 on 12/28/91; geophysical. Research of magnetosphere nad the ionosphere of the Earth by passive and active methods. Launched on 18 Dec 1991. The Czechoslovak satellite Magion 3 forms, together with the spacecraft Intercosmos 25, part of the Apex scientific project. Magion 3 was sep arated into an autonomous orbit on 28 Dec 1991. Magion 3 was launched into orbit by the Soviet spacecraft Intercosmos 25.

1992 December 22 - . 12:36 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 2226 - . Payload: Geo-IK no. 13. Mass: 1,500 kg (3,300 lb). Nation: Russia. Agency: MO. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 22282 . COSPAR: 1992-092A. Apogee: 1,525 km (947 mi). Perigee: 1,479 km (919 mi). Inclination: 73.6000 deg. Period: 116.00 min. Summary: Investigation of outer space. .

1994 May 25 - . 10:15 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. FAILURE: Stage 2 and 3 failed to separate due to a breakdown of the launch vehicle control system.. Failed Stage: 3.
  • Tselina-D - . Payload: Tselina-D no. 74. Nation: Russia. Agency: VKS. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. COSPAR: F940525A. Summary: Destroyed by launch safety..

1994 October 11 - . 14:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Okean-O1 no. 7 - . Payload: Okean-O1 no. 7. Mass: 1,950 kg (4,290 lb). Nation: Russia. Agency: RAKA. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. USAF Sat Cat: 23317 . COSPAR: 1994-066A. Apogee: 665 km (413 mi). Perigee: 631 km (392 mi). Inclination: 82.5400 deg. Period: 97.70 min. Summary: Oceanography..

1994 November 29 - . 02:54 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Geo-IK - . Payload: Geo-IK no. 14. Mass: 1,500 kg (3,300 lb). Nation: Russia. Agency: RAKA. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 23411 . COSPAR: 1994-078A. Apogee: 1,526 km (948 mi). Perigee: 1,481 km (920 mi). Inclination: 73.6000 deg. Period: 116.10 min. Summary: Also tested Elekon communcations payload..

1994 December 26 - . 22:26 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. Launch Pad: LC32/2?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 2299 - . Payload: Strela-3 no. 99. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 23441 . COSPAR: 1994-086A. Apogee: 1,415 km (879 mi). Perigee: 1,402 km (871 mi). Inclination: 82.5700 deg. Period: 113.97 min. Summary: Six satellites launched by a single carrier rocket..
  • Cosmos 2304 - . Payload: Strela-3 no. 104. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 23446 . COSPAR: 1994-086F. Apogee: 1,417 km (880 mi). Perigee: 1,412 km (877 mi). Inclination: 82.5600 deg. Period: 114.11 min.
  • Cosmos 2300 - . Payload: Strela-3 no. 100. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 23442 . COSPAR: 1994-086B. Apogee: 1,414 km (878 mi). Perigee: 1,410 km (870 mi). Inclination: 82.5500 deg. Period: 114.05 min.
  • Cosmos 2303 - . Payload: Strela-3 no. 103. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 23445 . COSPAR: 1994-086E. Apogee: 1,430 km (880 mi). Perigee: 1,413 km (877 mi). Inclination: 82.5600 deg. Period: 114.26 min.
  • Cosmos 2302 - . Payload: Strela-3 no. 102. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 23444 . COSPAR: 1994-086D. Apogee: 1,423 km (884 mi). Perigee: 1,414 km (878 mi). Inclination: 82.6000 deg. Period: 114.20 min.
  • Cosmos 2301 - . Payload: Strela-3 no. 101. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 23443 . COSPAR: 1994-086C. Apogee: 1,415 km (879 mi). Perigee: 1,414 km (878 mi). Inclination: 82.5600 deg. Period: 114.11 min.

2001 July 31 - . 08:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Koronas-F - . Payload: AUOS-SM-KF. Mass: 2,260 kg (4,980 lb). Nation: Russia. Agency: RAKA. Manufacturer: Yuzhnoye. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: AUOS. Decay Date: 2005-12-06 . USAF Sat Cat: 26873 . COSPAR: 2001-032A. Apogee: 529 km (328 mi). Perigee: 486 km (301 mi). Inclination: 82.5000 deg. Launch delayed from July 25. Koronas-F was a Russian solar observatory that pointed toward Sun within 10 arc-minutes to conduct a variety of observations. In broad categories, it carried X-ray monitors to locate sources within 1 arc-sec, radio receivers to measure flux and polarization, and particle counters. Additional Details: here....

2004 December 24 - . 11:20 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. LV Configuration: Tsiklon-3 701. FAILURE: Launch vehicle control system failure during third stage apogee kick burn..
  • Sich-1M - . Payload: Okean O1-N9. Mass: 2,263 kg (4,989 lb). Nation: Ukraine. Agency: NKAU. Manufacturer: Yuzhnoye. Program: Okean. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Okean-O1. Decay Date: 2006-04-15 . USAF Sat Cat: 28505 . COSPAR: 2004-052A. Apogee: 650 km (400 mi). Perigee: 280 km (170 mi). Inclination: 82.5559 deg. Summary: Ukranian-built remote sensing satellite. Originally tagged by USAF SpaceCom as Cosmos 2412. Third stage apogee kick burn was too short, raising the perigee of the orbit from 78 km to 280 km, rather than the 650 km planned..
  • Mikron - . Payload: MK-1TS. Mass: 66 kg (145 lb). Nation: Ukraine. Agency: NKAU. Manufacturer: Yuzhnoye. Class: Technology. Type: Navigation technology satellite. Spacecraft: MS-1. Decay Date: 2005-09-30 . USAF Sat Cat: 28507 . COSPAR: 2004-052C. Apogee: 650 km (400 mi). Perigee: 280 km (170 mi). Inclination: 82.5559 deg. The Mikron microsatellite was equipped with a small visible range video camera. The information from the satellite was to be used to provide remote sensing of topography and meteorology. However the main purpose of the experimental satellite was to test the MS-1 microsatellite bus created under the Ukrainian National Space Program. The satellites spectral range was from 0.45 to 0.90 mm; swath width was 253-391 km; resolution 124-191 m.

2009 January 30 - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Koronas-Foton - . Payload: AUOS-SM-KF. Mass: 1,900 kg (4,100 lb). Nation: Russia. Agency: RAKA. Manufacturer: Yuzhnoye. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: AUOS. USAF Sat Cat: 33504 . COSPAR: 2009-003A. Apogee: 561 km (348 mi). Perigee: 539 km (334 mi). Inclination: 82.5000 deg. Period: 95.70 min. Carried ten instruments to study in the sun throughout the electromagnetic spectrum, primarily Russian: Natalya-2M spectrometer; RT-2 gamma-telescope (India); Pingvin-M polarimeter; Konus-RF x-ray and gamma spectrometer; BRM x-ray detector; FOKA UV-detector; TESIS telescope/spectrometer with SphinX soft X-ray spectrophotometer (Poland); Electron-M-Peska charged particles analyser; STEP-F Electron and proton detector(Ukraine); SM-8M magnetometer. Follow-up to 2001 Koronas-F launch.

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