Encyclopedia Astronautica
RKA


Russian Space Agency

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Associated Countries
Associated Spacecraft
  • 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...

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RKA Chronology


1998 July 10 - . 06:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2.
  • WESTPAC - . Mass: 24 kg (52 lb). Nation: Australia. Agency: WPLTN. Manufacturer: RKA; EOS. Class: Earth. Type: Geodetic satellite. Spacecraft: GFZ-1. USAF Sat Cat: 25398 . COSPAR: 1998-043E. Apogee: 819 km (508 mi). Perigee: 815 km (506 mi). Inclination: 98.8000 deg. Period: 101.20 min. Formerly known as WPLTN-1, this geodesy satellite was a copy of Potsdam's GFZ-1 satellite, a sphere covered with laser retroreflectors, with a different `Fizeau' corner cube design. It serves as a target for the Western Pacific Laser Tracking Network (WPLTN) and is a joint project of Electro Optic Systems of Queanbeyan, New South Wales, Australia, and the Russian Space Agency. Diameter is 0.24m.

2004 October 14 - . 03:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG Zh15000-012.
  • Soyuz TMA-5 - . Call Sign: Tien Shan. Crew: Chiao; Sharipov; Shargin. Return Crew: Chiao; Sharipov; Vittori. Payload: Soyuz TMA s/n 215. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Chiao; Sharipov; Shargin; Vittori. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-10. Spacecraft: Soyuz TMA. Duration: 192.79 days. Decay Date: 2005-04-25 . USAF Sat Cat: 28444 . COSPAR: 2004-040A. Apogee: 359 km (223 mi). Perigee: 353 km (219 mi). Inclination: 51.6000 deg. Period: 91.70 min. Soyuz TMA-5 docked with the Pirs module on October 16 at 0416 GMT. Aboard the spacecraft were the EO-10 crew of Sharipov and Chiao, and guest cosmonaut Shargin. After a week at the station, the EO-9 crew of Padalka and Fincke, together with Shargin, entered Soyuz TMA-4 at 18:14 GMT on October 23 and returned to earth. Chiao and Sharipov continued as the ISS skeleton station crew.

2005 February 28 - . 19:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 093 / ISS-17P.
  • Nanosputnik - . Payload: TEKh-42 / TNS-0 s/n 1. Mass: 5.00 kg (11.00 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Technology. Type: Navigation technology satellite. Flight: ISS EO-10. Spacecraft: Nanosputnik. Decay Date: 2005-08-30 . USAF Sat Cat: 28547 . COSPAR: 2005-007C. Apogee: 353 km (219 mi). Perigee: 341 km (211 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: Nanosatellite delivered by Progress M-52 to the International Space Station. 30 cm long, it was released from during a spacewalk on 28 March 2005..

2005 April 15 - . 00:45 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG Zh15000-014 / ISS-10S.
  • Soyuz TMA-6 - . Call Sign: Basalt. Crew: Krikalyov; Phillips; Vittori. Return Crew: Krikalyov; Phillips; Olsen. Payload: Soyuz TMA s/n 216. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Vittori; Krikalyov; Phillips; Olsen. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-11; ISS EP-8; ISS EO-10. Spacecraft: Soyuz TMA. Duration: 179.02 days. Decay Date: 2005-10-11 . USAF Sat Cat: 28640 . COSPAR: 2005-013A. Apogee: 360 km (220 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. The Soyuz TMA-6 docked with International Space Station's Pirs module at 02:20 GMT on April 17. Commander of the long-duration EO-11 crew was Russian cosmonaut Sergey Krikalyov. Flight engineer and science officer was American astronaut John Phillips. Italian Roberto Vittori accompanied the EO-10 crew aboard Soyuz TMA-6 to the station on the European Space Agency EP-8 Eneide mission.

2006 October 19 - . 16:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz ST. LV Configuration: Soyuz-2-1A/Fregat Zh15000-003/ST16.
  • Metop-A - . Mass: 4,093 kg (9,023 lb). Nation: Europe. Agency: RKA. Class: Earth. Type: Weather satellite. Spacecraft: Metop. USAF Sat Cat: 29499 . COSPAR: 2006-044A. Apogee: 817 km (507 mi). Perigee: 817 km (507 mi). Inclination: 98.7000 deg. Period: 101.00 min. European polar weather satellite equipped with high-resolution visible and infrared cameras, a microwave sounder, ozone monitors, a GPS atmospheric sounding device, a wind scatterometer, and a search and rescue package. First launch of the Soyuz 2 version of the venerable Soyuz launch vehicle. The main change in this first version of the new booster was a digital control system. Problems with this system delayed the launch repeatedly.

2007 October 10 - . 13:22 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG Ts15000-020.
  • Soyuz TMA-11 - . Call Sign: Agat. Crew: Whitson; Malenchenko; Muszaphar. Payload: Soyuz TMA s/n 221 / ISS 15S. Mass: 7,200 kg (15,800 lb). Nation: Russia. Related Persons: Whitson; Malenchenko; Muszaphar. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-16; ISS EP-13. Spacecraft: Soyuz TMA. Duration: 191.80 days. Decay Date: 2008-04-19 . USAF Sat Cat: 32256 . COSPAR: 2007-045A. Apogee: 344 km (213 mi). Perigee: 340 km (210 mi). Inclination: 51.6000 deg. Period: 91.40 min. Soyuz TMA-11 delivered the EO-16 crew of Whitson and Malenchenko and EP-13 space tourist Shukor to the International Space Station. The Soyuz docked at the Zarya module at 14:50 GMT on 12 October. Whitson was EO-16 commander, with third astronaut Clay Anderson remaining aboard the station after the EO-15 crew and Shukor returned to earth on Soyuz TMA-10.

    Malenchenko and Whitson, together with visiting Korean astronaut Yi, who had been delivered to the ISS by Soyuz TMA-12, undocked from the station aboard Soyuz TMA-11 at 05:06 GMT on 19 April 2008. Following the deorbit burn at 07:40 GMT the aft service module of the Soyuz failed to separate and the spacecraft began re-entry in a reversed position, with the forward hatch taking the initial re-entry heating. As was the case with Soyuz 5 in 1970, the connections with the service module finally melted away, and the freed capsule righted itself aerodynamically with the heat shield taking the brunt of the re-entry heating. However the crew experienced a rough ride, a ballistic re-entry of over 8 G's force, smoke in the cabin, a failure of the soft landing system, and a very hard landing. They landed 470 km short of the target point at 50 deg 31" N, 61 deg 7" E at 08:29 GMT. A small grass fire was started at the landing point and the injured crew had to be helped from the capsule by passers-by. Malenchenko and Whitson suffered no permanent injury, but Yi was hit by Whitson's personal effects bag on impact and required physical therapy for neck and spine injuries.


2008 February 5 - . 13:03 GMT - . Launch Site: Baikonur. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1730.
  • Progress M-63 - . Payload: Progress M s/n 363. Mass: 7,130 kg (15,710 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-16; ISS EO-16-1. Spacecraft: Progress M. Duration: 61.96 days. Decay Date: 2008-04-07 12:00:00 . USAF Sat Cat: 32484 . COSPAR: 2008-004A. Apogee: 339 km (210 mi). Perigee: 338 km (210 mi). Inclination: 51.6000 deg. Period: 91.30 min. Summary: Docked with the ISS at the Pirs module on 7 February at 14:38 GMT. Undocked on 7 April at 08:49 GMT and was deorbited over the Pacific later the same day..

2008 April 8 - . 11:16 GMT - . Launch Site: Baikonur. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz FG s/n 1731.
  • Soyuz TMA-12 - . Call Sign: Eridanus. Crew: Volkov, Sergey; Kononenko, O D; Yi So-yeon. Return Crew: Volkov, Sergey; Kononenko, O D; Garriott, Richard. Payload: Soyuz TMA s/n 222. Mass: 7,200 kg (15,800 lb). Nation: Russia. Related Persons: Volkov, Sergey; Kononenko, O D; Yi So-yeon; Garriott, Richard. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-16; ISS EO-17; ISS EO-16-3. Spacecraft: Soyuz TMA. Duration: 198.54 days. Decay Date: 2008-04-19 08:29:00 . USAF Sat Cat: 32756 . COSPAR: 2008-015A. Apogee: 343 km (213 mi). Perigee: 336 km (208 mi). Inclination: 51.6000 deg. Period: 91.30 min. Launched the EO-17 long-duration crew to replace the EO-16 crew. The commander was the son of cosmonaut Aleksandr Volkov. Also aboard was Oleg Kononenko (no relation to the 1970's Buran pilot of the same name) and Korean astronaut Yi Soyeon. Soyuz TMA-12 docked at the Pirs module of the International Space Station on 2008 Apr 10 at 12:57 GMT on 10 April. Volkov and Kononenko stayed aboard as the EO-17 long duration crew. Yi returned to earth with the EO-16 crew aboard Soyuz TMA-11. Soyuz TMA-12 undocked on 24 October at 00:16 GMT with the EO-17 crew of Kononenko and Volkov, plus space tourist Richard Garriott, aboard. They landed safely at 03:37 GMT.

2008 May 14 - . 20:23 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1733.
  • Progress M-64 - . Payload: Progress M s/n 364. Mass: 7,056 kg (15,555 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-17; ISS EO-16-3. Spacecraft: Progress M. Duration: 137.02 days. Decay Date: 2008-09-08 . USAF Sat Cat: 32847 . COSPAR: 2008-023A. Apogee: 343 km (213 mi). Perigee: 336 km (208 mi). Inclination: 51.6000 deg. Period: 91.30 min. Unmanned space station resupply mission. Docked with the International Space Station at the Zarya port on 16 May. Undocked on 1 September at 19:47 GMT. It then flew for a week in independent orbit, carrying out the Plazma-Progress experiment. On 8 September at 20:47 GMT it was deorbited to destruction over the Pacific Ocean.

2008 September 10 - . 19:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1735.
  • Progress M-65 - . Payload: Progress M s/n 365. Mass: 7,100 kg (15,600 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-17; ISS EO-17-1. Spacecraft: Progress M. Duration: 88.00 days. Decay Date: 2008-12-07 . USAF Sat Cat: 33340 . COSPAR: 2008-043A. Apogee: 357 km (221 mi). Perigee: 348 km (216 mi). Inclination: 51.6000 deg. Period: 91.60 min. Docking with the ISS at the Zvezda module was delayed due to NASA Houston operations being curtailed during Hurricane Ike. The resupply spacecraft finally docked at 18:43 GMT on 27 September. It undocked at 16:20 GMT on 14 November, but then flew independently in orbit until 7 December in order to conduct continue ionospheric experiments.

2008 October 12 - . 07:01 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz FG s/n 1736.
2008 November 26 - . 12:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1738.
  • Progress M-01M - . Payload: Progress M s/n 401. Mass: 7,290 kg (16,070 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-18; ISS EO-18-1. Spacecraft: Progress M. Duration: 74.00 days. Decay Date: 2009-02-08 . USAF Sat Cat: 33443 . COSPAR: 2008-060A. Apogee: 362 km (224 mi). Perigee: 352 km (218 mi). Inclination: 51.6000 deg. Period: 91.70 min. Summary: ISS resupply spacecraft, a modernized version of Progress with a digital control system, docked at the Pirs port of the station on 30 November..

2009 February 10 - . 05:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1740.
  • Progress M-66 - . Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Flight: ISS EO-18; ISS EO-18-1. Spacecraft: Progress M. Duration: 97.00 days. Decay Date: 2009-05-18 . USAF Sat Cat: 33593 . COSPAR: 2009-006A. Apogee: 357 km (221 mi). Perigee: 342 km (212 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: ISS resupply. Docked with the ISS at 07:18 GMT on 13 February. Undocked at 15:18 on 6 May and destroyed over the Pacific on 18 May..

2009 March 26 - . 11:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG s/n 1741.
  • Soyuz TMA-14 - . Call Sign: Altair. Crew: Padalka; Barratt; Simonyi. Payload: Soyuz TMA s/n 224. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-19. Spacecraft: Soyuz TMA. Duration: 198.66 days. Decay Date: 2009-10-11 . USAF Sat Cat: 34669 . COSPAR: 2009-015A. Apogee: 354 km (219 mi). Perigee: 344 km (213 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: Delivered EO-19 crew and space tourist Simonyi to ISS; returned EO-19 crew and space tourist Laliberte to earth on 11 October 2009 at 04:32 GMT..

2009 May 7 - . 18:37 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1743.
  • Progress M-02M - . Mass: 7,120 kg (15,690 lb). Nation: Russia. Agency: RKA. Program: ISS. Flight: ISS EO-19. Spacecraft: Progress M. Duration: 67.00 days. Decay Date: 2009-07-13 . USAF Sat Cat: 34905 . COSPAR: 2009-024A. Apogee: 348 km (216 mi). Perigee: 337 km (209 mi). Inclination: 51.6000 deg. Period: 91.40 min. ISS logistics flight. Docked with the Pirs module of the ISS on 12 May at 19:24. Undocked with ISS on 30 June, conducted scientific experiments, then made a second rendezvous with the ISS at the Zvezda module to test docking systems for the upcoming Mini-Research Module 2. Backed away after getting within 10 m of the station. Retrofire on 13 July followed by burn up over the Pacific at 16:28 GMT.

2009 May 27 - . 10:34 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG s/n 1745.
  • Soyuz TMA-15 - . Call Sign: Parus. Crew: Romanenko, Roman; De Winne; Thirsk. Payload: Soyuz TMA s/n 225. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-20; ISS EO-19. Spacecraft: Soyuz TMA. Duration: 187.86 days. Decay Date: 2009-12-01 . USAF Sat Cat: 35010 . COSPAR: 2009-030A. Apogee: 354 km (219 mi). Perigee: 344 km (213 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: Delivered EO-20 crew to the ISS. Returned to earth 1 December 2009..

2009 July 24 - . 10:56 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1/5. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1746.
  • Progress M-67 - . Mass: 7,285 kg (16,060 lb). Nation: Russia. Agency: RKA. Program: ISS. Flight: ISS EO-20; ISS EO-19. Spacecraft: Progress M. Duration: 65.00 days. Decay Date: 2009-09-27 . USAF Sat Cat: 35641 . COSPAR: 2009-040A. Apogee: 354 km (219 mi). Perigee: 344 km (213 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: Docked at the Zvezda port of the International Space Station at 11:12 GMT on 29 July. Undocked and was deorbited over the Pacific Ocean on 27 September at 09:33 GMT..

2009 September 17 - . 15:55 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz ST / Fregat ST. LV Configuration: Soyuz-2-1b/Fregat.
  • IRIS - . Nation: Russia. Agency: RKA. Class: Technology. Type: Technology satellite. USAF Sat Cat: 35867 . COSPAR: 2009-049C. Apogee: 502 km (311 mi). Perigee: 490 km (300 mi). Inclination: 97.3000 deg. Period: 94.50 min. Summary: Inflatable structure technology test - two inflatable masts carrying dummy solar arrays..
  • BLITS - . Mass: 7.00 kg (15.40 lb). Nation: Russia. Agency: RKA. Class: Earth. Type: Earth resources satellite. USAF Sat Cat: 35871 . COSPAR: 2009-049G. Apogee: 822 km (510 mi). Perigee: 818 km (508 mi). Inclination: 98.8000 deg. Period: 101.30 min. Summary: Spherical glass lens for laser geodesy, built by the NII for Precision Instruments (NIIPP), Moscow..
  • Sumbandila - . Mass: 81 kg (178 lb). Nation: Russia. Agency: RKA. Class: Technology. Type: Technology satellite. USAF Sat Cat: 35870 . COSPAR: 2009-049F. Apogee: 505 km (313 mi). Perigee: 501 km (311 mi). Inclination: 97.3000 deg. Period: 94.70 min. Summary: South African imaging satellite with a ground resolution of 6.25 m..
  • Meteor-M - . Mass: 2,700 kg (5,900 lb). Nation: Russia. Agency: RKA. Class: Earth. Type: Weather satellite. Spacecraft: Meteor-M. USAF Sat Cat: 35865 . COSPAR: 2009-049A. Apogee: 820 km (500 mi). Perigee: 818 km (508 mi). Inclination: 98.8000 deg. Period: 101.30 min. First Meteor-M satellite. This replaced the Meteor-3M satellite, with new generation weather instruments. Plagued with problems: the infrared sensor cooling broke down, an antenna did not deploy properly, camera mirrors were degraded by vibration, imagery was not delivered in a usable rectified format.

2009 September 30 - . 07:14 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG s/n 1748.
  • Soyuz TMA-16 - . Call Sign: Bort. Crew: Surayev; Williams, Jeffrey; Laliberte. Payload: Soyuz TMA s/n 226. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-21; ISS EO-20; ISS EO-19. Spacecraft: Soyuz TMA. Duration: 169.17 days. Decay Date: 2010-03-18 . USAF Sat Cat: 35940 . COSPAR: 2009-053A. Apogee: 352 km (218 mi). Perigee: 342 km (212 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: Docked with the International Space Station at 08:35 GMT on 2 October. Carried the EO-21 crew of Suraev and Williams, and space tourist Guy Laliberte due to the station. Surayev and Williams landed aboard Soyuz TMA-16 in Kazakhstan on 18 March 2010..

2009 October 15 - . 01:14 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1749.
  • Progress M-03M - . Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-21; ISS EO-20. Spacecraft: Progress M. Decay Date: 2010-05-03 . USAF Sat Cat: 35948 . COSPAR: 2009-056A. Apogee: 348 km (216 mi). Perigee: 314 km (195 mi). Inclination: 51.6000 deg. Period: 91.20 min. Summary: Docked at the Pirs module of the International Space Station at 01:41 GMT on 18 October..

2009 November 10 - . 14:22 GMT - . Launch Site: Baikonur. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Poisk - . Payload: Progress M s/n 302 / 240GK s/n 2L. Mass: 3,670 kg (8,090 lb). Nation: Russia. Agency: RKA. Spacecraft: Progress M-SO. USAF Sat Cat: 36086 . COSPAR: 2009-060A. Perigee: 11 km (6 mi). Docking/research module for the ISS, consisting of a pressurized Small Research Module and a Progress M service module. Docked at the zenith port of the Zvezda module of the ISS at 15:41 GMT on 12 November. On 8 December at 00:16 GMT the service module separated from Small Research Module, leaving the docking port clear for future spacecraft visiting the ISS. At 04:48 GMT the service module retrofired into a descructive reentry over the Pacific at 05:27 GMT.

2009 December 20 - . 21:52 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1752.
  • Soyuz TMA-17 - . Call Sign: Pulsar. Crew: Kotov; Creamer; Noguchi. Backup Crew: Wheelock; Shkaplerov; Furukawa. Payload: Soyuz 7K-STMA s/n 227 / ISS-21S. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Kotov; Creamer; Noguchi. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-22; ISS EO-21. Spacecraft: Soyuz TMA. Duration: 163.23 days. Decay Date: 2010-06-02 . USAF Sat Cat: 36129 . COSPAR: 2009-074A. Apogee: 351 km (218 mi). Perigee: 336 km (208 mi). Inclination: 51.6000 deg. Period: 91.40 min. Summary: Docked with Zarya port of ISS at 22:48 GMT on 22 December. Undocked at 0:04 GMT on 2 June 2010 and landed in Kazakhstan at 03:25 GMT..

2010 February 3 - . 03:45 GMT - . Launch Site: Baikonur. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1753.
  • Progress M-04M - . Mass: 7,400 kg (16,300 lb). Nation: Russia. Agency: RKA. Program: ISS. Flight: ISS EO-22; ISS EO-21. Spacecraft: Progress M. Duration: 148.42 days. Decay Date: 2010-07-01 . USAF Sat Cat: 36361 . COSPAR: 2010-003A. Apogee: 353 km (219 mi). Perigee: 346 km (214 mi). Inclination: 51.6000 deg. Period: 91.50 min. Summary: Undocked from the Zvezda module of the ISS on 10 May 2010. Conducted free-flight experiments until deorbited at 13:54 GMT on 1 July..

2010 April 2 - . 04:04 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG s/n 1754.
  • Soyuz TMA-18 - . Call Sign: Cliff. Crew: Skvortsov, Aleksandr; Korniyenko; Caldwell. Backup Crew: Borisenko, Andrei; Samokutyayev; Kelly, Scott. Payload: Soyuz 7K-STMA s/n 228. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-23; ISS EO-22. Spacecraft: Soyuz TMA. Duration: 176.05 days. Decay Date: 2010-04-20 . USAF Sat Cat: 36505 . COSPAR: 2010-011A. Apogee: 361 km (224 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. ISS EO-23. The crew first attempted to depart the ISS on 24 September. However the latches between the Soyuz and the station failed to release. Return to earth the next day was successful, with undocking at 02:03 GMT; deorbit burn at 04:31 GMT; and landing in Kazakhstan at 05:23 GMT.

2010 April 28 - . 17:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1756.
  • Progress M-05M - . Mass: 7,400 kg (16,300 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-23; ISS EO-23; ISS EO-22. Spacecraft: Progress M. Duration: 201.00 days. Decay Date: 2010-11-15 . USAF Sat Cat: 36521 . COSPAR: 2010-018A. Apogee: 361 km (224 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. Summary: Undocked from the Pirs module of the ISS on 25 October 2010 at 14:22 GMT and was deorbited over the Pacific on 15 November 2010 after three weeks of independent flight..

2010 June 15 - . 21:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG s/n 1757.
  • Soyuz TMA-19 - . Call Sign: Olympus. Crew: Yurchikhin; Wheelock; Walker, Shannon. Backup Crew: Kondratiyev, Dmitry; Nespoli; Coleman. Payload: Soyuz 7K-STMA s/n 229. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-24; ISS EO-23. Spacecraft: Soyuz TMA. Duration: 163.30 days. Decay Date: 2010-11-26 . USAF Sat Cat: 36603 . COSPAR: 2010-029A. Apogee: 361 km (224 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. ISS EO-24 crew. The return to earth was reported advanced four days to avoid coinciding with an OSCE conference in Kazakhstan. The crew undocked from the Rassvet module of the ISS at 01:23 GMT on 26 November 2010. There was a leak in the descent module, but ground controllers concluded the return to earth could be conducted safely. The Soyuz made its deorbit burn at 03:55 GMT and landed safely in Kazakhstan at 04:46 GMT.

2010 June 30 - . 15:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n 1758.
  • Progress M-06M - . Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-24; ISS EO-23. Spacecraft: Progress M. Duration: 67.86 days. Decay Date: 2010-07-14 . USAF Sat Cat: 36748 . COSPAR: 2010-033A. Apogee: 361 km (224 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. First docking attempt with the ISS on 2 July aborted due to radio interference. Successfully docked with the ISS at the Zvezda module on 4 July at 16:17 GMT. Undocked from the Zvezda module of the ISS at 11:21 GMT on 31 August 2010. Conducted experiments in free flight until deorbited at 12:13 GMT on 6 September.

2010 September 10 - . 10:22 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Progress M-07M - . Payload: Progress M-07M. Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-24; ISS EO-23. Spacecraft: Progress M. Duration: 163.00 days. Decay Date: 2011-02-20 . USAF Sat Cat: 37156 . COSPAR: 2010-044A. Apogee: 355 km (220 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. Summary: Docked at the Zvezda module of the ISS at 11:58 GMT on 12 September 2010. Undocked from Zvezda on 20 February 2011 at 13:12 GMT and deorbited over the Pacific at 16:12 GMT..

2010 October 7 - . 23:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG.
  • Soyuz TMA-01M - . Call Sign: Ingul. Crew: Kaleri; Skripochka; Kelly, Scott. Payload: Soyuz TMA-01M. Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-25; ISS EO-24. Spacecraft: Soyuz TMA. Duration: 159.78 days. Decay Date: 2011-03-16 . USAF Sat Cat: 37183 . COSPAR: 2010-052A. Apogee: 355 km (220 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. Summary: ISS EO-25 crew. The Soyuz docked at the Poisk module of the ISS at 00:01 GMT on 10 October. The crew entered the spacecraft and undocked at 04:27 GMT on 16 March 2011. Following retrofire and re-entry they landed safely in Kazakhstan at 07:53 GMT..

2010 October 19 - . 17:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton/Briz M.
  • Globalstar M079 - . Payload: Globalstar-2 M079. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37188 . COSPAR: 2010-054A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min. Summary: First six or 48 new-generation Globalstar-2 satellites that will replace the 44 operational Globalstar satellites already aloft..
  • Globalstar M074 - . Payload: Globalstar-2 M074. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37189 . COSPAR: 2010-054B. Apogee: 1,415 km (879 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.
  • Globalstar M076 - . Payload: Globalstar-2 M076. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37190 . COSPAR: 2010-054C. Apogee: 1,415 km (879 mi). Perigee: 1,412 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.
  • Globalstar M077 - . Payload: Globalstar-2 M077. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37191 . COSPAR: 2010-054D. Apogee: 993 km (617 mi). Perigee: 951 km (590 mi). Inclination: 52.0000 deg. Period: 104.50 min.
  • Globalstar M075 - . Payload: Globalstar-2 M075. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37192 . COSPAR: 2010-054E. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.
  • Globalstar M073 - . Payload: Globalstar-2 M073. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37193 . COSPAR: 2010-054F. Apogee: 1,004 km (623 mi). Perigee: 955 km (593 mi). Inclination: 52.0000 deg. Period: 104.70 min.

2010 October 27 - . 15:11 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Progress M-08M - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-25; ISS EO-24. Spacecraft: Progress M. Duration: 88.59 days. Decay Date: 2011-01-24 . USAF Sat Cat: 37196 . COSPAR: 2010-055A. Apogee: 355 km (220 mi). Perigee: 352 km (218 mi). Inclination: 51.6000 deg. Period: 91.60 min. Summary: Undocked from the Pirs module of the ISS at 00:42 GMT on 24 January 2011 and deorbited over the Pacific at 05:16 GMT the same day..

2010 December 15 - . 19:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG.
  • Soyuz TMA-20 - . Call Sign: Varyag. Crew: Kondratiyev, Dmitry; Nespoli; Coleman. Backup Crew: Ivanishin; Furukawa; Fossum. Payload: Soyuz 7K-STMA s/n 230. Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-26; ISS EO-25. Spacecraft: Soyuz TMA. Duration: 159.30 days. Decay Date: 2011-05-24 . USAF Sat Cat: 37254 . COSPAR: 2010-067A. Apogee: 355 km (220 mi). Perigee: 350 km (210 mi). Inclination: 51.6000 deg. Period: 91.60 min. ISS EO-26 crew. Docked at the Rassvet module of the ISS at 20:11 GMT on 17 December. The crew boarded Soyuz TMA-20 and undocked at 21:35 GMT on 23 May 2011. They pulled back 200 m from the station, then took comprehensive photography of the station until 22:17 as it rotated before them. After departure from the visinity of the station, the Soyuz fired its engines at 01:36 GMT on 24 May to start the descent into the atmosphere. The orbital module and service modules separated from the descent module at 02:01 GMT. The crew landed safely in Kazakhstan at 02:27 GMT.

2011 April 4 - . 22:18 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG.
  • Soyuz TMA-21 - . Call Sign: Tarkhany / Gagarin. Crew: Samokutyayev; Borisenko; Garan. Backup Crew: Shkaplerov; Ivanishin; Burbank. Payload: Soyuz 7K-STMA s/n 231. Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-27; ISS EO-26. Spacecraft: Soyuz TMA. Duration: 164.24 days. Decay Date: 2011-09-16 . USAF Sat Cat: 37382 . COSPAR: 2011-012A. Apogee: 347 km (215 mi). Perigee: 343 km (213 mi). Inclination: 51.6000 deg. Period: 91.40 min. ISS EO-27 crew. The Soyuz docked at the Poisk module of the ISS at 23:09 GMT on 6 April, and undocked at 00:38 GMT on 16 September 2011, eight days later than planned due to the Progress M-11M launch failure. A dropout of communications after the reentry burn caused concern, but the crew landed safely in Kazakhstan at 03:59 GMT.

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