 | Tselina-D Credit - Yuzhnoye
| Article Number: 11F619. Code Name: Ikar. Class: SIGINT. Destination: Medium Earth Orbit. Nation: Ukraine. Agency: MOM. Manufacturer: Yuzhnoye. The Tselina D was the detailed observation portion of the two-satellite Tselina ELINT satellite system. Development began in the 1960's, with first launch in 1970, but major technical difficulties resulted in the Tselina-D not being declared operational until 1976. However by 1984 technical improvements allowed Tselina-D to take over the general surveillance function of the other satellite. The final launch attempt in the series took place in 1994.
The Tselina dedicated ELINT satellite system included two satellites: Tselina-O for general surveillance and Tselina-D for detailed observations. TsNII-108 GKRE (Zaslavskiy) developed the payload while V M Kovtunenko of Yuzhnoye/OKB-586 build the satellite and launch vehicle.
The first Tselina-O was launched by a Kosmos-3M in 1970. Delays in payload development and weight growth in the Tselina-D resulted in the whole Tselina system not being operational until 1976. The Vostok booster had to be used due to the higher weight of Tselina-D; this was later replaced by the Tsyklon-3 booster. Constant improvement resulted in Tselina-O being abandoned in 1984 and all systems being put on Tselina-D. In 1981 a second control and information processing center was established.
Tselina-D and -O spacecraft were operated simultaneously to maximize results. The Tselina system not only localized and classified radio emitters but also characterized their functional regimes. It also characterized command traffic from military units, allowing targeting of those units by photo reconnaissance satellites.
Tselina-D satellites were operated in six orbital planes, spaced 30 degrees apart. They would record data received, and then dump it to ground stations while passing over the Soviet Union. In the late 1980's the much larger Tselina-2, launched by a Zenit-2 booster, began taking over the task. The last successful Tselina-D launch was in 1992. By that time the constellation had been reduced to three orbital planes spaced at 60 degrees, complementing the Zenit-2 constellation in four higher-altitude orbital planes spaced 40 degrees apart.
Western observers could monitor the status of the Tselina-D satellites via their continuous-wave beacons which operated at 153 MHz.
Typical orbit: 544 km x 566 km at 82 degrees inclination.
Tselina-D Chronology - 1970 January 2 - Tsiklon 3 launch vehicle development authorised. - Launch Vehicle: Tsiklon.
Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On the Creation of the Carrier-Rocket 11K68 on The Basis of 11K69 RN and S5M Stage for Launch of Space Apparatus 'Tselina' and .Meteor'--approval of work on the Tsiklon-3 RN
- 1970 December 18 - Cosmos 389 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 543 km (337 mi). Apogee: 568 km (352 mi). Inclination: 81.20 deg. Period: 95.80 min.
- 1971 April 7 - Cosmos 405 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 594 km (369 mi). Apogee: 603 km (374 mi). Inclination: 81.20 deg. Period: 96.70 min.
- 1972 March 1 - Cosmos 476 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 379 km (235 mi). Apogee: 388 km (241 mi). Inclination: 81.20 deg. Period: 92.20 min.
- 1972 December 28 - Cosmos 542 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 527 km (327 mi). Apogee: 640 km (390 mi). Inclination: 81.00 deg. Period: 96.30 min.
- 1973 October 29 - Cosmos 604 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,000 kg (4,400 lb). Perigee: 413 km (256 mi). Apogee: 424 km (263 mi). Inclination: 81.20 deg. Period: 92.90 min.
- 1974 August 16 - Cosmos 673 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 399 km (247 mi). Apogee: 416 km (258 mi). Inclination: 81.20 deg. Period: 92.70 min.
- 1975 June 20 - Cosmos 744 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 367 km (228 mi). Apogee: 380 km (230 mi). Inclination: 81.20 deg. Period: 92.00 min.
- 1975 August 22 - Cosmos 756 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 394 km (244 mi). Apogee: 403 km (250 mi). Inclination: 81.20 deg. Period: 92.50 min.
- 1976 March 16 - Cosmos 808 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,000 kg (6,600 lb). Perigee: 363 km (225 mi). Apogee: 370 km (220 mi). Inclination: 81.20 deg. Period: 91.90 min.
- 1976 August 27 - Cosmos 851 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,000 kg (6,600 lb). Perigee: 300 km (180 mi). Apogee: 313 km (194 mi). Inclination: 81.20 deg. Period: 90.70 min.
- 1976 December 10 - Tselina-D accepted for military service. -
Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On adoption of the Tselina-D into armaments' was issued.
- 1977 February 26 - Cosmos 895 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 433 km (269 mi). Apogee: 442 km (274 mi). Inclination: 81.20 deg. Period: 93.30 min.
- 1977 June 24 - Cosmos 921 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/2. Launch Vehicle: Tsiklon. Mass: 5,000 kg (11,000 lb). Perigee: 587 km (364 mi). Apogee: 651 km (404 mi). Inclination: 75.80 deg. Period: 97.10 min.
Launch vehicle test. Dummy payload. Investigation of the upper atmosphere and outer space.
- 1977 July 7 - Cosmos 925 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 269 km (167 mi). Apogee: 275 km (170 mi). Inclination: 81.20 deg. Period: 90.00 min.
- 1977 September 20 - Cosmos 955 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 493 km (306 mi). Apogee: 501 km (311 mi). Inclination: 81.20 deg. Period: 94.60 min.
- 1977 September 24 - Cosmos 956 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/2. Launch Vehicle: Tsiklon. FAILURE: Probable failure of launch vehicle stage to reach proper orbit. Mass: 5,000 kg (11,000 lb). Perigee: 355 km (220 mi). Apogee: 864 km (536 mi). Inclination: 75.80 deg. Period: 96.80 min.
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 - Cosmos 972 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/2. Launch Vehicle: Tsiklon. FAILURE: Probable failure of launch vehicle stage to reach proper orbit. Mass: 5,000 kg (11,000 lb). Perigee: 712 km (442 mi). Apogee: 1,157 km (718 mi). Inclination: 75.80 deg. Period: 103.70 min.
Launch vehicle test. Dummy payload. Probable failure of launch vehicle stage to reach proper orbit. Investigation of the upper atmosphere and outer space.
- 1978 January 10 - Cosmos 975 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 513 km (318 mi). Apogee: 522 km (324 mi). Inclination: 81.20 deg. Period: 95.00 min.
- 1978 May 12 - Cosmos 1005 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 485 km (301 mi). Apogee: 494 km (306 mi). Inclination: 81.20 deg. Period: 94.40 min.
- 1978 June 28 - Cosmos 1025 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/2. Launch Vehicle: Tsiklon. Mass: 4,375 kg (9,645 lb). Perigee: 551 km (342 mi). Apogee: 567 km (352 mi). Inclination: 82.50 deg. Period: 95.80 min.
- 1978 October 10 - Cosmos 1043 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 425 km (264 mi). Apogee: 433 km (269 mi). Inclination: 81.20 deg. Period: 93.20 min.
- 1978 December 19 - Cosmos 1063 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 518 km (321 mi). Apogee: 524 km (325 mi). Inclination: 81.20 deg. Period: 95.10 min.
- 1979 February 13 - Cosmos 1077 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 485 km (301 mi). Apogee: 491 km (305 mi). Inclination: 81.20 deg. Period: 94.40 min.
- 1979 April 14 - Cosmos 1093 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 474 km (294 mi). Apogee: 487 km (302 mi). Inclination: 81.20 deg. Period: 94.20 min.
- 1979 July 20 - Cosmos 1116 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 396 km (246 mi). Apogee: 408 km (253 mi). Inclination: 81.20 deg. Period: 92.60 min.
- 1979 October 26 - Cosmos 1143 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 524 km (325 mi). Apogee: 533 km (331 mi). Inclination: 81.30 deg. Period: 95.20 min.
- 1979 November 27 - Cosmos 1145 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 4,000 kg (8,800 lb). Perigee: 484 km (300 mi). Apogee: 495 km (307 mi). Inclination: 81.20 deg. Period: 94.40 min.
- 1980 January 30 - Cosmos 1154 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 540 km (330 mi). Apogee: 545 km (338 mi). Inclination: 81.20 deg. Period: 95.50 min.
- 1980 March 18 - Tselina-D - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Vehicle: Soyuz. FAILURE: Booster exploded on pad during servicing. Severe pad damage, 48 people killed. Cause found to be change in solder with tin to that with lead in H2O2 filters, causing decomposition and explosion.
This was the worst disaster since the Nedelin Catastrophe on 24 October 1964. A commission of military officers and chief designers reviewed the incident and requested changes to equipment and procedures, especially as regarded liquid oxygen handling. Another source reports that the explosion occurred during the fuelling of the Block E upper stage, and was due to hydrogen peroxide being present in a lox line filter and a confusion between fuel and lox lines. This error had always been possible, but had never happened in the 20 years of use of the booster before the explosion. The launch pad was badly damaged and not put back into service until April 1983.
- 1980 June 4 - Cosmos 1184 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 532 km (330 mi). Apogee: 535 km (332 mi). Inclination: 81.20 deg. Period: 95.30 min.
- 1980 August 15 - Cosmos 1206 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 525 km (326 mi). Apogee: 531 km (329 mi). Inclination: 81.20 deg. Period: 95.20 min.
- 1980 November 21 - Cosmos 1222 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 3,800 kg (8,300 lb). Perigee: 557 km (346 mi). Apogee: 561 km (348 mi). Inclination: 81.20 deg. Period: 95.90 min.
- 1981 January 27 - Cosmos 1242 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 568 km (352 mi). Apogee: 584 km (362 mi). Inclination: 81.20 deg. Period: 96.20 min.
- 1981 May 19 - Cosmos 1271 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 565 km (351 mi). Apogee: 582 km (361 mi). Inclination: 81.20 deg. Period: 96.20 min.
Replaced Cosmos 1077.
- 1981 August 24 - Cosmos 1300 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/1. Launch Vehicle: Tsiklon. Perigee: 589 km (365 mi). Apogee: 609 km (378 mi). Inclination: 82.50 deg. Period: 96.70 min.
- 1981 October 13 - Cosmos 1315 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 571 km (354 mi). Apogee: 599 km (372 mi). Inclination: 81.20 deg. Period: 96.40 min.
Replaced Cosmos 1154.
- 1981 December 3 - Cosmos 1328 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/1. Launch Vehicle: Tsiklon. Perigee: 597 km (370 mi). Apogee: 619 km (384 mi). Inclination: 82.50 deg. Period: 96.90 min.
- 1982 February 19 - Cosmos 1340 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 590 km (360 mi). Apogee: 604 km (375 mi). Inclination: 81.20 deg. Period: 96.60 min.
Replaced Cosmos 1206.
- 1982 March 31 - Cosmos 1346 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 572 km (355 mi). Apogee: 602 km (374 mi). Inclination: 81.20 deg. Period: 96.40 min.
Replaced Cosmos 1222.
- 1982 May 5 - Cosmos 1356 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 587 km (364 mi). Apogee: 612 km (380 mi). Inclination: 81.20 deg. Period: 96.70 min.
Replaced Cosmos 1184.
- 1982 June 10 - Cosmos 1378 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/1. Launch Vehicle: Tsiklon. Mass: 2,200 kg (4,800 lb). Perigee: 593 km (368 mi). Apogee: 618 km (384 mi). Inclination: 82.50 deg. Period: 96.80 min.
- 1982 August 5 - Cosmos 1400 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 575 km (357 mi). Apogee: 590 km (360 mi). Inclination: 81.20 deg. Period: 96.30 min.
Replaced Cosmos 1315.
- 1982 September 16 - Cosmos 1408 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,200 kg (4,800 lb). Perigee: 587 km (364 mi). Apogee: 617 km (383 mi). Inclination: 82.60 deg. Period: 96.70 min.
Replaced Cosmos 1378.
- 1983 January 20 - Cosmos 1437 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 2,500 kg (5,500 lb). Perigee: 581 km (361 mi). Apogee: 604 km (375 mi). Inclination: 81.20 deg. Period: 96.50 min.
- 1983 February 16 - Cosmos 1441 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Vehicle: Soyuz. Mass: 2,000 kg (4,400 lb). Perigee: 578 km (359 mi). Apogee: 587 km (364 mi). Inclination: 81.10 deg. Period: 96.30 min.
- 1983 April 23 - Cosmos 1455 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 592 km (367 mi). Apogee: 617 km (383 mi). Inclination: 82.50 deg. Period: 96.80 min.
- 1983 June 22 - Cosmos 1470 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 596 km (370 mi). Apogee: 626 km (388 mi). Inclination: 82.50 deg. Period: 96.90 min.
- 1983 December 15 - Cosmos 1515 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 595 km (369 mi). Apogee: 620 km (380 mi). Inclination: 82.50 deg. Period: 96.90 min.
- 1984 February 8 - Cosmos 1536 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,200 kg (4,800 lb). Perigee: 602 km (374 mi). Apogee: 631 km (392 mi). Inclination: 82.50 deg. Period: 97.00 min.
- 1984 March 15 - Cosmos 1544 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 591 km (367 mi). Apogee: 618 km (384 mi). Inclination: 82.50 deg. Period: 96.80 min.
- 1984 October 18 - Cosmos 1606 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 592 km (367 mi). Apogee: 623 km (387 mi). Inclination: 82.50 deg. Period: 96.90 min.
Replaced Cosmos 1455.
- 1985 January 24 - Cosmos 1626 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,200 kg (4,800 lb). Perigee: 590 km (360 mi). Apogee: 618 km (384 mi). Inclination: 82.50 deg. Period: 96.80 min.
Replaced Cosmos 1408.
- 1985 March 5 - Cosmos 1633 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,200 kg (4,800 lb). Perigee: 595 km (369 mi). Apogee: 613 km (380 mi). Inclination: 82.50 deg. Period: 96.80 min.
Replaced Cosmos 1470.
- 1985 July 8 - Cosmos 1666 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,500 kg (3,300 lb). Perigee: 595 km (369 mi). Apogee: 622 km (386 mi). Inclination: 82.50 deg. Period: 96.90 min.
- 1985 August 8 - Cosmos 1674 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,500 kg (3,300 lb). Perigee: 594 km (369 mi). Apogee: 620 km (380 mi). Inclination: 82.50 deg. Period: 96.80 min.
Replaced Cosmos 1536.
- 1985 November 22 - Cosmos 1703 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 596 km (370 mi). Apogee: 621 km (385 mi). Inclination: 82.50 deg. Period: 96.90 min.
Replaced Cosmos 1674.
- 1985 December 12 - Cosmos 1707 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 596 km (370 mi). Apogee: 623 km (387 mi). Inclination: 82.50 deg. Period: 96.90 min.
Replaced Cosmos 1515.
- 1986 January 17 - Cosmos 1726 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 590 km (360 mi). Apogee: 618 km (384 mi). Inclination: 82.50 deg. Period: 96.80 min.
- 1986 February 19 - Cosmos 1733 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 594 km (369 mi). Apogee: 618 km (384 mi). Inclination: 82.50 deg. Period: 96.80 min.
Replaced Cosmos 1544.
- 1986 May 15 - Cosmos 1743 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 594 km (369 mi). Apogee: 623 km (387 mi). Inclination: 82.60 deg. Period: 96.90 min.
Replaced Cosmos 1626.
- 1986 June 12 - Cosmos 1758 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 603 km (374 mi). Apogee: 636 km (395 mi). Inclination: 82.50 deg. Period: 97.10 min.
Replaced Cosmos 1666.
- 1986 September 30 - Cosmos 1782 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,400 kg (3,000 lb). Perigee: 605 km (375 mi). Apogee: 628 km (390 mi). Inclination: 82.50 deg. Period: 97.00 min.
- 1986 December 10 - Cosmos 1805 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,400 kg (3,000 lb). Perigee: 598 km (371 mi). Apogee: 622 km (386 mi). Inclination: 82.50 deg. Period: 96.90 min.
- 1987 January 14 - Cosmos 1812 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 598 km (371 mi). Apogee: 622 km (386 mi). Inclination: 82.50 deg. Period: 96.90 min.
Ocean surveillance.
- 1987 March 3 - Cosmos 1825 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 594 km (369 mi). Apogee: 621 km (385 mi). Inclination: 82.50 deg. Period: 96.80 min.
Ocean surveillance.
- 1987 April 27 - Cosmos 1842 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 602 km (374 mi). Apogee: 628 km (390 mi). Inclination: 82.50 deg. Period: 97.00 min.
- 1987 July 1 - Cosmos 1862 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 602 km (374 mi). Apogee: 636 km (395 mi). Inclination: 82.50 deg. Period: 97.10 min.
- 1987 October 20 - Cosmos 1892 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 595 km (369 mi). Apogee: 623 km (387 mi). Inclination: 82.50 deg. Period: 96.90 min.
- 1988 January 6 - Cosmos 1908 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 600 km (370 mi). Apogee: 626 km (388 mi). Inclination: 82.50 deg. Period: 97.00 min.
- 1988 March 15 - Cosmos 1933 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 605 km (375 mi). Apogee: 629 km (390 mi). Inclination: 82.50 deg. Period: 97.10 min.
- 1988 June 14 - Cosmos 1953 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 1,600 kg (3,500 lb). Perigee: 604 km (375 mi). Apogee: 637 km (395 mi). Inclination: 82.50 deg. Period: 97.10 min.
Outer space research.
- 1988 October 11 - Cosmos 1975 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Perigee: 604 km (375 mi). Apogee: 636 km (395 mi). Inclination: 82.50 deg. Period: 97.10 min.
Investigation of outer space.
- 1990 January 30 - Cosmos 2058 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 616 km (382 mi). Apogee: 645 km (400 mi). Inclination: 82.50 deg. Period: 97.30 min.
Investigation of outer space.
- 1991 June 13 - Cosmos 2151 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 625 km (388 mi). Apogee: 653 km (405 mi). Inclination: 82.50 deg. Period: 97.50 min.
Investigation of outer space.
- 1992 November 24 - Cosmos 2221 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 630 km (390 mi). Apogee: 662 km (411 mi). Inclination: 82.50 deg. Period: 97.70 min.
Investigation of outer space.
- 1992 December 25 - Cosmos 2228 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 628 km (390 mi). Apogee: 666 km (413 mi). Inclination: 82.50 deg. Period: 97.70 min.
Investigation of outer space.
- 1993 April 16 - Cosmos 2242 - Program: Tselina. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Tsiklon. Mass: 2,000 kg (4,400 lb). Perigee: 629 km (390 mi). Apogee: 665 km (413 mi). Inclination: 82.50 deg. Period: 97.70 min.
Ocean surveillance. Investigation of outer space.
- 1994 May 25 - Tselina-D - Program: Tselina. Launch Site: Plesetsk. Launch Complex: LC32/2. Launch Vehicle: Tsiklon. FAILURE: Stage 2 and 3 failed to separate due to a breakdown of the launch vehicle control system.
Destroyed by launch safety.
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- Krebs, Gunter, Gunter's Space Page, University of Frankfurt, 1996. Web Address when accessed: http://www.skyrocket.de/space.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- Voevodin, Sergey A, VSA072 - Space Apparatus, "Sergey A. Voevodin's Reports", Web Address when accessed: http://home.attbi.com/~rusaerog/spacecraft.html.
- Melnik, T G, Voenno-Kosmicheskiy Siliy, Nauka, Moscow, 1997..
- Siddiqi, Asif A, The Soviet Space Race With Apollo, University Press of Florida, 2003.
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