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RKA
Russian Space Agency, Moscow, Russia.

AKA: Rossiskoe aviatsionno-kosmicheskoe agentsvo (Rosaviakosmos). Location: Moskva.



Country: Russia. Spacecraft: Okean-O1.

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: EOS, RKA. 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.
  • Soyuz TMA-5 - . Call Sign: Tien Shan. Crew: Chiao, Shargin, Sharipov. Return Crew: Chiao, Sharipov, Vittori. Payload: Soyuz TMA s/n 215. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Chiao, Shargin, Sharipov, Vittori. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-5. Spacecraft Bus: Soyuz. 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-U-PVB.
  • 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: Soyuz TMA-5. 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. 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.
  • Soyuz TMA-6 - . Call Sign: Basalt. Crew: Krikalyov, Phillips, Vittori. Return Crew: Krikalyov, Olsen, Phillips. Payload: Soyuz TMA s/n 216. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Krikalyov, Olsen, Phillips, Vittori. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-5, Soyuz TMA-6, Soyuz TMA-6 Eneide. Spacecraft Bus: Soyuz. 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-2-1A.
  • Metop-A - . Mass: 4,093 kg (9,023 lb). Nation: Europe. Agency: RKA. Class: Earth. Type: Weather satellite. Spacecraft Bus: SPOT-5A-5B. 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.
  • Soyuz TMA-11 - . Call Sign: Agat. Crew: Malenchenko, Muszaphar, Whitson. Payload: Soyuz TMA s/n 221 / ISS 15S. Mass: 7,200 kg (15,800 lb). Nation: Russia. Related Persons: Malenchenko, Muszaphar, Whitson. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-11, Soyuz TMA-11 ISS EP-13. Spacecraft Bus: Soyuz. 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-U-PVB.
  • 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: Soyuz TMA-11, STS-120 ISS EO-16. Spacecraft Bus: Soyuz. 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. 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.
  • Soyuz TMA-12 - . Call Sign: Eridanus. Crew: Kononenko, Volkov, Sergey, Yi Soyeon. Return Crew: Garriott, Richard, Kononenko, Volkov, Sergey. Payload: Soyuz TMA s/n 222. Mass: 7,200 kg (15,800 lb). Nation: Russia. Related Persons: Garriott, Richard, Kononenko, Volkov, Sergey, Yi Soyeon. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-12, STS-123 ISS EO-16. Spacecraft Bus: Soyuz. 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-U-PVB.
  • 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: Soyuz TMA-12, STS-123 ISS EO-16. Spacecraft Bus: Soyuz. 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-U-PVB.
  • 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: Soyuz TMA-12, STS-124 ISS EO-17. Spacecraft Bus: Soyuz. 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.
  • Soyuz TMA-13 - . Call Sign: Titan. Crew: Fincke, Garriott, Richard, Lonchakov. Payload: Soyuz TMA s/n 223. Mass: 7,200 kg (15,800 lb). Nation: Russia. Related Persons: Fincke, Garriott, Richard, Lonchakov. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-13. Spacecraft Bus: Soyuz. Spacecraft: Soyuz TMA. Duration: 178.01 days. Decay Date: 2009-04-08 . USAF Sat Cat: 33399 . COSPAR: 2008-050A. Apogee: 362 km (224 mi). Perigee: 352 km (218 mi). Inclination: 51.6000 deg. Period: 91.70 min. Docked at the Zarya port of the ISS on 14 October at 08:26 GMT..

2008 November 26 - . 12:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • 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: Soyuz TMA-13, STS-126 ISS EO-18. Spacecraft Bus: Soyuz. 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. 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-U-PVB.
  • Progress M-66 - . Payload: Progress M s/n 366. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-13, STS-126 ISS EO-18. Spacecraft Bus: Soyuz. 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. 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.
  • Soyuz TMA-14 - . Call Sign: Altair. Crew: Barratt, Padalka, Simonyi. Backup Crew: Dyson, Surayev, Walker. Return Crew: Barratt, Laliberte, Padalka. 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: Soyuz TMA-14. Spacecraft Bus: Soyuz. 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. 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-U-PVB.
  • Progress M-02M - . Payload: Progress M s/n 402. Mass: 7,120 kg (15,690 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-14. Spacecraft Bus: Soyuz. 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.
  • Soyuz TMA-15 - . Call Sign: Parus. Crew: De Winne, Romanenko, Roman, Thirsk. Backup Crew: Hadfield, Kondratiyev, Kuipers. 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: Soyuz TMA-15. Spacecraft Bus: Soyuz. 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. 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. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-67 - . Payload: Progress M s/n 367. Mass: 7,285 kg (16,060 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-14, Soyuz TMA-15. Spacecraft Bus: Soyuz. 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. 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-2-1B.
  • Meteor-M - . Mass: 2,700 kg (5,900 lb). Nation: Russia. Agency: RKA. Class: Earth. Type: Weather satellite. Spacecraft Bus: Meteor. 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.

  • 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. Inflatable structure technology test - two inflatable masts carrying dummy solar arrays mounted on the Fregat upper stage and inflated after all payloads had been deployed..
  • Sumbandila - . Mass: 81 kg (178 lb). Nation: Russia. Agency: RKA. Class: Technology. Type: Technology satellite. Spacecraft: Sumbandila. 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. South African imaging satellite with a ground resolution of 6.25 m..
  • BLITS - . Mass: 7.00 kg (15.40 lb). Nation: Russia. Agency: RKA. Class: Earth. Type: Earth resources satellite. Spacecraft: BLITS. 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. Spherical glass lens for laser geodesy, built by the NII for Precision Instruments (NIIPP), Moscow..

2009 September 30 - . 07:14 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-FG.
  • Soyuz TMA-16 - . Call Sign: Bort. Crew: Laliberte, Surayev, Williams, Jeffrey. Backup Crew: Barrett, Skvortsov, Walker, Shannon. Return Crew: Surayev, Williams. 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: Soyuz TMA-16. Spacecraft Bus: Soyuz. 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. 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-U-PVB.
  • Progress M-03M - . Payload: Progress M s/n 403. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-15, Soyuz TMA-16. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 194.00 days. 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. 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-U-PVB.
  • Poisk - . Payload: Progress M s/n 302 / 240GK s/n 2L. Mass: 3,670 kg (8,090 lb). Nation: Russia. Agency: RKA. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. 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-FG.
  • Soyuz TMA-17 - . Call Sign: Pulsar. Crew: Creamer, Kotov, Noguchi. Backup Crew: Furukawa, Shkaplerov, Wheelock. Payload: Soyuz 7K-STMA s/n 227 / ISS-21S. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Creamer, Kotov, Noguchi. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-17. Spacecraft Bus: Soyuz. 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. 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. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-04M - . Payload: Progress M s/n 404 / ISS-36P. Mass: 7,400 kg (16,300 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-16, Soyuz TMA-17. Spacecraft Bus: Soyuz. 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. 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.
  • Soyuz TMA-18 - . Call Sign: Cliff. Crew: Caldwell, Korniyenko, Skvortsov, Aleksandr. Backup Crew: Borisenko, Andrei, Kelly, Scott, Samokutyayev. 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: Soyuz TMA-18. Spacecraft Bus: Soyuz. 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-U-PVB.
  • Progress M-05M - . Payload: Progress M s/n 405 / ISS-37P. Mass: 7,400 kg (16,300 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-17, Soyuz TMA-18, Soyuz TMA-18. Spacecraft Bus: Soyuz. 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. 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.
  • Soyuz TMA-19 - . Call Sign: Olympus. Crew: Walker, Shannon, Wheelock, Yurchikhin. Backup Crew: Coleman, Catherine, Kondratiyev, Nespoli. 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: Soyuz TMA-19. Spacecraft Bus: Soyuz. 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-U-PVB.
  • Progress M-06M - . Payload: Progress M s/n 406 / ISS-38P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-18, Soyuz TMA-19. Spacecraft Bus: Soyuz. 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-U-PVB.
  • Progress M-07M - . Payload: Progress M s/n 407 / ISS-39P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-18, Soyuz TMA-19. Spacecraft Bus: Soyuz. 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. 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, Kelly, Scott, Skripochka. Backup Crew: Garan, Kononenko, Volkov, Sergey. Payload: Soyuz TMA s/n 701. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-01M. Spacecraft Bus: Soyuz. 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. 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 LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.
  • Globalstar M079 - . Payload: Globalstar-2 M079. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian 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. 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: Civilian 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: Civilian 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: Civilian 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: Civilian 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: Civilian 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-U-PVB.
  • Progress M-08M - . Payload: Progress M s/n 408 / ISS-40P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-01M, Soyuz TMA-19. Spacecraft Bus: Soyuz. 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. 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: Coleman, Catherine, Kondratiyev, Nespoli. Backup Crew: Fossum, Furukawa, Ivanishin. Payload: Soyuz 7K-STMA s/n 230. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-20. Spacecraft Bus: Soyuz. 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 January 28 - . 01:31 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-09M - . Payload: Progress M s/n 409 / ISS-41P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-01M, Soyuz TMA-20. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 88.00 days. Decay Date: 2011-04-26 . USAF Sat Cat: 37359 . COSPAR: 2011-004A. Apogee: 345 km (214 mi). Perigee: 270 km (160 mi). Inclination: 51.6000 deg. Period: 90.70 min. Undocked from the Pirs module of the ISS on 22 April at 11:41 GMT and deorbited over the Pacific on 26 April..

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: Borisenko, Garan, Samokutyayev. Backup Crew: Burbank, Ivanishin, Shkaplerov. Payload: Soyuz 7K-STMA s/n 231. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-21. Spacecraft Bus: Soyuz. 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.


2011 April 27 - . 13:05 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-10M - . Payload: Progress M s/n 410 / ISS-42P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-20, Soyuz TMA-21. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 185.00 days. Decay Date: 2011-10-29 . USAF Sat Cat: 37396 . COSPAR: 2011-017A. Apogee: 347 km (215 mi). Perigee: 343 km (213 mi). Inclination: 51.6000 deg. Period: 91.40 min. Docked with the ISS Pirs module at 14:28 GMT on 29 April. Undocked at 09:04 GMT on 29 October. Following retrofire at 12:10 GMT it was destroyed on reentry over the Pacific at 12:48 GMT..

2011 June 21 - . 14:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-11M - . Payload: Progress M s/n 411 / ISS-43P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-02M, Soyuz TMA-21. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 71.79 days. Decay Date: 2011-09-01 . USAF Sat Cat: 37679 . COSPAR: 2011-027A. Apogee: 383 km (237 mi). Perigee: 343 km (213 mi). Inclination: 51.6000 deg. Period: 91.80 min.

    ISS resupply. Also carried the 40 kg Chibis satellite. Docked with the Zvezda module of the ISS on 23 June at 16:37 GMT. Undocked from Zvezda at 09:38 GMT on 23 August. After several maneuvers to carry out the Radar-4 experiment, deorbited over the Pacific at 09:34 GMT on 1 September.


2011 August 24 - . 13:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB. FAILURE: Five minutes and 25 seconds into flight, during the burn of the booster's third stage, the engine's gas generator failed and the engine shut down. The upper stage and spacecraft crashed in the Gorno-Altai region.. Failed Stage: 3.
  • Progress M-12M - . Payload: Progress M s/n 412 / ISS-44P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-02M, Soyuz TMA-21. Spacecraft Bus: Soyuz. Spacecraft: Progress M.

    ISS resupply mission. The Progress M failed to reach orbit. Five minutes and 25 seconds into flight, during the burn of the booster's third stage, the engine's gas generator failed and the engine shut down. The upper stage and spacecraft crashed in the Gorno-Altai region of Russia. First ever failure of a Progress spacecraft to dock with a space station in its 135-mission history. The six crew aboard the ISS had sufficient supplies, but the mishap delayed the launch of the Expedition 29 replacement crew until the cause of the failure was understood and the Soyuz launch vehicle cleared again for manned launches. The return to Earth of the first half of the Expedition 28 crew has also delayed to mid-September, meaning the station would be reduced to a three-person crew for a time.


2011 October 30 - . 10:11 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-13M - . Payload: Progress M s/n 413 / ISS-45P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: Soyuz TMA-02M. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 87.00 days. Decay Date: 2012-01-25 . USAF Sat Cat: 37857 . COSPAR: 2011-062A. Apogee: 403 km (250 mi). Perigee: 374 km (232 mi). Inclination: 51.6000 deg. Period: 92.30 min.

    Space station resupply. Docked with the Pirs module of the ISS on 2 November. This restored resupply of the station after the Progress M-12M launch failure and two intermediate successful flights of the Soyuz booster. Also carried the Chibis-M subsatellite.


2011 November 14 - . 04:14 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-FG.
  • Soyuz TMA-22 - . Call Sign: Astraeus. Crew: Burbank, Ivanishin, Shkaplerov. Backup Crew: Acaba, Padalka, Revin. Payload: Soyuz 7K-STMA s/n 232. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-22. Spacecraft Bus: Soyuz. Spacecraft: Soyuz TMA. Duration: 165.31 days. Decay Date: 2012-04-27 . USAF Sat Cat: 37877 . COSPAR: 2011-067A. Apogee: 410 km (250 mi). Perigee: 376 km (233 mi). Inclination: 51.6000 deg. Period: 92.40 min.

    Launch delayed two months to verify booster after launch failure of Progress M-12M in August 2011. After successful launch of Progress M-13M on 30 October, Soyuz TMA-22 was cleared for launch. Delivered the EO-29 crew to the ISS, docking at the Poisk module of the station at 05:24 GMT on 16 November. Undocked on 27 April 2012 at 08:15 GMT and landed in Kazakhstan at 11:45 GMT.


2012 January 25 - . 23:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-14M - . Payload: Progress M s/n 414 / ISS-46P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 94.00 days. Decay Date: 2012-04-28 . USAF Sat Cat: 38073 . COSPAR: 2012-004A. Apogee: 405 km (251 mi). Perigee: 375 km (233 mi). Inclination: 51.6000 deg. Period: 92.40 min. Docked with the International Space Station at the Pirs module on 28 January at 00:09 GMT. Undocked on 19 April 11:04 GMT to begin nine days of autonomous Radar-Progress ionospheric experiments. Deorbited over the Pacific Ocean on 28 April..

2012 April 20 - . 12:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-15M - . Payload: Progress M s/n 415 / ISS-47P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 122.00 days. Decay Date: 2012-08-20 . USAF Sat Cat: 38222 . COSPAR: 2012-015A. Apogee: 406 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.6000 deg. Period: 92.50 min.

    Docked at the Pirs module of the International Space Station on 22 April at 14:39 GMT. Undocked and after three weeks of independent flight involving Radar-Progress experiments using thruster burns to study the ionosphere, was deorbited over the Pacific on 20 August.


2012 August 1 - . 19:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-16M - . Payload: Progress M s/n 416 / ISS-48P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 192.00 days. Decay Date: 2013-02-09 . USAF Sat Cat: 38738 . COSPAR: 2012-042A. Apogee: 428 km (265 mi). Perigee: 403 km (250 mi). Inclination: 51.6000 deg. Period: 92.90 min. Undocked from the Pirs module at 13:16 GMT on 9 February. Deorbited over the Pacific Ocean at 16:19 GMT with debris impact at 17:05 GMT..

2012 October 31 - . 07:41 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
  • Progress M-17M - . Payload: Progress M s/n 417 / ISS-49P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 172.00 days. Decay Date: 2013-04-21 . USAF Sat Cat: 38975 . COSPAR: 2012-060A. Apogee: 422 km (262 mi). Perigee: 401 km (249 mi). Inclination: 51.6000 deg. Period: 92.80 min.

    Docked with the Zvezda module of the ISS after a quick-rendezvous 5 hour 52 min flight. Undocked from Zvezda at 12:02 GMT on 15 April for independent flight to conduct Radar-Progress ionospheric tests. Retrofire on 21 April on 14:07 GMT lasted 173 seconds, producing a delta-V of 90 m/s. Impacted in the Pacific at 15:02 GMT.


2013 February 11 - . 14:41 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-18M - . Payload: Progress M s/n 418 / ISS-50P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 165.00 days. Decay Date: 2013-07-26 . USAF Sat Cat: 39082 . COSPAR: 2013-007A. Apogee: 421 km (261 mi). Perigee: 409 km (254 mi). Inclination: 51.6500 deg. Period: 92.88 min. Docked with the Pirs module of the ISS at 20:34 GMT on launch day. Undocked from the Pirs module at 20:53 GMT on July 25 and was deorbited over the South Pacific three hours later, with debris ocean impact around 00:42 GMT July 26..

2013 April 24 - . 10:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-19M - . Payload: Progress M s/n 419 / ISS-51P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 56.00 days. Decay Date: 2013-06-19 . USAF Sat Cat: 39148 . COSPAR: 2013-017A. Apogee: 418 km (259 mi). Perigee: 360 km (220 mi). Inclination: 51.6500 deg. Period: 92.34 min.

    Although one of the spacecraft's rendezvous antennae did not deploy, it docked successfully with the aft port of the ISS Zvezda module at 12:25 GMT on 26 April. Undocked from the Zvezda module at 13:58 GMT on 11 June to clear the port for the ATV resupply vehicle. Maneuvered to a 416 km x 456 km orbit for Radar-Progress ionospheric experiments.


2013 July 27 - . 20:45 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-20M - . Payload: Progress M s/n 420 / ISS-52P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 199.00 days. Decay Date: 2014-02-11 . USAF Sat Cat: 39219 . COSPAR: 2013-039A. Apogee: 414 km (257 mi). Perigee: 361 km (224 mi). Inclination: 51.6500 deg. Period: 92.30 min.

    Docked with the Pirs module of the ISS 5 hr 41 min after launch. Payload delivered to the station included a 1U cubesat, Chasqui 1 from Peru's Universidad Nacional de Ingenieria. Undocked from the Pirs module of the ISS at 16:21 GMT on 3 February 2014. Deorbited on February 11 following a week of independent operations, with impact in the South Pacifc at 15:55 GMT.


2013 November 25 - . 20:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-21M - . Payload: Progress M s/n 421 / ISS-53P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 196.00 days. Decay Date: 2014-06-09 . USAF Sat Cat: 39456 . COSPAR: 2013-069A. Apogee: 418 km (259 mi). Perigee: 412 km (256 mi). Inclination: 51.6500 deg. Period: 92.87 min.

    It made a 1.5 km flyby of ISS at 21:50 GMT on November 27 to test the new Kurs-NA rendezvous system, and then a re-rendezvous on November 29. A glitch forced a switch to manual TORU control for the last 60 m to docking with the Zvezda module at 22:30 GMT. Undocked from Zvezda on June 9 at 13:30 GMT and was deorbited the same day, with debris falling in the South Pacific around 17:23 GMT.


2014 February 5 - . 16:23 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-22M - . Payload: Progress M s/n 422 / ISS-54P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 72.00 days. Decay Date: 2014-04-18 . USAF Sat Cat: 39506 . COSPAR: 2014-005A. Apogee: 418 km (259 mi). Perigee: 361 km (224 mi). Inclination: 51.6500 deg. Period: 92.34 min.

    ISS mission 54P; docked at the Pirs module of the ISS at 22:22 GMT the same day as launch. Undocked from the Pirs module at 13:58 GMT April 7; it remained in a 360 x 417 km orbit for Radar-Progress ionospheric studies until April 18, when it was deorbited over the Pacific.


2014 April 9 - . 15:26 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-23M - . Payload: Progress M s/n 427 / ISS-55P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 113.00 days. Decay Date: 2014-07-31 . USAF Sat Cat: 39648 . COSPAR: 2014-018A. Apogee: 417 km (259 mi). Perigee: 412 km (256 mi). Inclination: 51.6500 deg. Period: 92.85 min.

    Docked with the Pirs module of the ISS at 21:14 GMT the same day as launch. Undocked from at 21:44 GMT on July 21 and then carried out 10 days of independent operations as part of the Radar-Progress experiment program. Deorbited on July 31 with impact at 22:43 GMT in the South Pacific.


2014 July 23 - . 21:44 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-24M - . Payload: Progress M s/n 423 / ISS-56P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 120.00 days. Decay Date: 2014-11-20 . USAF Sat Cat: 40097 . COSPAR: 2014-042A. Apogee: 419 km (260 mi). Perigee: 413 km (256 mi). Inclination: 51.6500 deg. Period: 92.89 min. Docked with the Pirs module of the ISS at 03:31 GMT on July 24. Undocked from Pirs at 05:38 GMT on October 27..

2014 October 29 - . 07:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1a.
  • Progress M-25M - . Payload: Progress M s/n 424 / ISS-57P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 179.00 days. Decay Date: 2015-04-26 . USAF Sat Cat: 40292 . COSPAR: 2014-067A. Apogee: 403 km (250 mi). Perigee: 396 km (246 mi). Inclination: 51.6400 deg. Period: 92.56 min. Docked with the ISS Pirs module at 13:08 GMT 29 October. Undocked from the Pirs module at 06:41 GMT on April 25 and was deorbited on April 26, with debris falling in the South Pacific at 13:00 GMT..

2015 February 17 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-26M - . Payload: Progress M s/n 426 / ISS-58P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Decay Date: 2015-08-14 . USAF Sat Cat: 40392 . COSPAR: 2015-008A. Apogee: 237 km (147 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg.

    Docked with the ISS Zvezda module at 16:57 GMT the same day as launched. Progress M-26M's engines were used to move the ISS out of the path of some space debris on 23 April and (following a malfunction on May 16) made an ISS orbit reboost on 18 May 18. Progress M-26M undocked 14 August at 10:19 GMT; was deorbited at 13:28 GMT; and impacted the Pacific around 141:7 GMT.


2015 April 28 - . 07:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1a. FAILURE: The third stage did not shut down correctly and damaged the spacecraft during separation.. Failed Stage: 3.
  • Progress M-27M - . Payload: Progress M s/n 425 / ISS-59P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 10.00 days. Decay Date: 2015-05-08 . USAF Sat Cat: 40619 . COSPAR: 2015-024A. Apogee: 258 km (160 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Limited telemetry was obtained from the Progress, but Russian mission control was unable to control the damaged, spinning spacecraft. The Progress reentered over the South Pacific off the southwest coast of Chile at 02:20 GMT on May 8..

2015 July 3 - . 14:21 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-28M - . Payload: Progress M s/n 428 / ISS-60P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Decay Date: 2015-12-19 . USAF Sat Cat: 40713 . COSPAR: 2015-031A. Apogee: 290 km (180 mi). Perigee: 262 km (162 mi). Inclination: 51.6300 deg. Period: 90.03 min.

    Carried critical supplies to the ISS after consecutive failures of all three primary resupply spacecraft to reach orbitů a prior Progress, a Cygnus, and a Dragon. Docking was at the Pirs module of the ISS on 5 July at 07:11 GMT. This launch used the older Soyuz-U rocket instead of the newer Soyuz-2-1a which ran into problems on the Progress M-27M launch. Undocked from Pirs at 0735 UTC Dec 19 and was deorbited over the South Pacific, with debris impact at 1128 UTC.


2015 October 1 - . 16:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress M-29M - . Mass: 7,283 kg (16,056 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Decay Date: 2016-04-08 . USAF Sat Cat: 40944 . COSPAR: 2015-055A. Apogee: 406 km (252 mi). Perigee: 398 km (247 mi). Inclination: 51.6500 deg. Period: 92.60 min.

    Docked with the ISS Zvezda module at 22:52 GMT on 1 October. The spacecraft delivered a variety of supplies and maintenance equipment to the station. Progress M-29M undocked from the Zvezda module on Mar 30 at 1415 UTC and performed attitude control experiments in a 373 x 401 km orbit. Progress M-29M was deorbited on Apr 8, reentered around 1416 UTC over the S Pacific.


2015 December 21 - . 08:44 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.
  • Progress MS-01 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. Decay Date: 2016-07-03 . USAF Sat Cat: 41177 . COSPAR: 2015-080A. Apogee: 279 km (173 mi). Perigee: 270 km (160 mi). Inclination: 51.6000 deg.

    First Progress-MS cargo ship. Progress-MS was similar to previous Progress ships but with improved onboard systems. It docked with the Pirs module at 1027 UTC Dec 23. Progress MS-01 undocked from the Pirs module at 0536 UTC on Jul 1, backed off to 180m, and redocked at 0605 UTC under TORU remote control. During redocking there was an incorrect thruster firing that made the vehicle swing visibly from side to side. The problem was reportedly under investigation but did not affect Progress MS-01's final undocking, which happened at 0348 UTC Jul 3. Progress MS-01 was deorbited and destroyed over the South Pacifc at 0750 UTC Jul 3.


2016 March 31 - . 16:23 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.
  • Progress MS-02 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. Decay Date: 2016-10-14 . USAF Sat Cat: 41436 . COSPAR: 2016-022A. Apogee: 267 km (165 mi). Perigee: 261 km (162 mi). Inclination: 51.6000 deg. Docked with Zvezda on Apr 2 at 1758 UTC..

2016 July 16 - . 21:41 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress MS-03 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. Decay Date: 2017-01-31 . USAF Sat Cat: 41670 . COSPAR: 2016-045A. Apogee: 225 km (139 mi). Perigee: 182 km (113 mi). Inclination: 51.6000 deg.

    Progress MS-03 cargo ship docked with the Pirs module at 0020 UTC Jul 19. It carried 2405 kg of cargo (including 705 kg of ISS propellant) as well as 880 kg of its own onboard propellant. Undocked at 1425 UTC and was deorbited at 1734 UTC with impact in the South Pacific at 1824 UTC.


2016 December 1 - . 14:51 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U. FAILURE: Third stage continued burning after payload separation.. Failed Stage: 3.
  • Progress MS-04 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. COSPAR: 2016-0F02. Apogee: 190 km (110 mi). Perigee: -4,000 km (-4,000 mi). Inclination: 51.6000 deg.

    The launch vehicle failed during third stage burn and its debris fell in the Tuva Republic. Lost with the rest of the cargo was the first Orlan-MKS spacesuit. Reports suggested the Progress separated from the rocket third stage prematurely and the accelerating stage then crashed into the Progress.


2017 February 22 - . 05:58 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Progress MS-05 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. USAF Sat Cat: 42056 . COSPAR: 2017-010A. Apogee: 210 km (130 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Launched of the final Soyuz-U-PVB rocket. Among other cargo the Progress cargo craft carried a new Orlan-MKS spacesuit. The ship docked with the Pirs module at 0830 UTC Feb 24..


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