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Soyuz-2-1B

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Soyuz-2-1B Part of R-7 Russian orbital launch vehicle. Incorporates digital flight control system from Soyuz-2-1A with new RD-0124 upper stage engine. AKA: 14A15. Status: Active. First Launch: 2006-12-27. Last Launch: 2018-11-03. Number: 28 . Thrust: 7,600.00 kN (1,708,500 lbf). Gross mass: 313,000 kg (690,000 lb). Height: 50.70 m (166.30 ft). Diameter: 2.95 m (9.67 ft). More at: Soyuz-2-1B. Family: orbital launch vehicle. Country: Russia. Spacecraft: BLITS, DX 1, Ekspress-1000, Persona, Relek, SkySat, Sterkh, Sumbandila , Tatyana, Toronto GNB, UGATUSAT , Meteor, Glonass, Yantar-4KS1, Resurs-Spektr, Cubesat, Meridian, Corot, SSTL-150, Meteor-M. Launch Sites: Baikonur, Plesetsk, Baikonur LC31, Plesetsk LC43/4, Plesetsk LC43. Stages: Fregat, Soyuz ST-0, Soyuz ST-1, Soyuz ST-2. Agency: Kozlov bureau. 2006 December 27 - . 14:23 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Corot - . Mass: 640 kg (1,410 lb). Nation: France. Agency: CNES. Manufacturer: Alenia. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft Bus: Proteus. Spacecraft: Corot. USAF Sat Cat: 29678 . COSPAR: 2006-063A. Apogee: 902 km (560 mi). Perigee: 898 km (557 mi). Inclination: 90.00 deg. Period: 103.00 min. European COnvection ROtation and planetary Transits satellite, designed to detect transits of planets down to earth size as they pass in front of their stars, and convection currents on stellar surfaces. The satellite was to use its 27-cm-diameter telescope to scan 120,000 stars during its 30-month mission. This was the first flight of the Soyuz-2 booster with the improved RD-0124 third stage engine. 2008 July 26 - . 18:31 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2441 - . Mass: 7,100 kg (15,600 lb). Nation: Russia. Agency: KVR. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Persona. USAF Sat Cat: 33272 . COSPAR: 2008-037A. Apogee: 735 km (456 mi). Perigee: 711 km (441 mi). Inclination: 98.30 deg. Period: 99.20 min. First in the Persona series of Russian military imaging reconnaisance satellites. The initial orbit was 195 x 726 km x 98.3 deg. The spacecraft maneuvered itself into its operational sun-synchronous orbit on 31 July. Reportedly the satellite married the Yantar electro-optical bus with subsystems developed for the abandoned Arkon-1 reconnsaisance satellite. Said to have shut down in February 2009 due to an electronics failure. 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: 98.80 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. Sterkh 12L - . Mass: 160 kg (350 lb). Nation: Russia. Class: Surveillance. Type: Search and rescue satellite. Spacecraft: Sterkh. USAF Sat Cat: 35866 . COSPAR: 2009-049B. Apogee: 818 km (508 mi). Perigee: 814 km (505 mi). Inclination: 98.54 deg. Period: 101.22 min. Second dedicated Sterkh search-and-rescue satellite.. 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: 97.30 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.. Tatyana-2 - . Mass: 90 kg (198 lb). Nation: Russia. Class: Science. Type: Science satellite. Spacecraft: Tatyana. USAF Sat Cat: 35868 . COSPAR: 2009-049D. Apogee: 820 km (500 mi). Perigee: 814 km (505 mi). Inclination: 98.54 deg. Period: 101.23 min. Space physics research satellite built by students from Moscow State University.. UGATUSAT - . Mass: 35 kg (77 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft: UGATUSAT. USAF Sat Cat: 35869 . COSPAR: 2009-049E. Apogee: 821 km (510 mi). Perigee: 815 km (506 mi). Inclination: 98.54 deg. Period: 101.25 min. Remote sensing satellite built by the Ufa State Aviation Technical University.. 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: 97.30 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: 98.80 deg. Period: 101.30 min. Spherical glass lens for laser geodesy, built by the NII for Precision Instruments (NIIPP), Moscow.. 2011 February 26 - . 03:07 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2471 - . Payload: Glonass-K No. 11. Mass: 1,415 kg (3,119 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Ekspress-1000. USAF Sat Cat: 37372 . COSPAR: 2011-009A. Apogee: 19,147 km (11,897 mi). Perigee: 19,111 km (11,875 mi). Inclination: 64.80 deg. Period: 675.70 min. First launch of the Glonass-K satellite using the Ekspress-1000 bus. The second would not come until 2014.. 2011 October 2 - . 20:15 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2474 - . Payload: Glonass-M No. 42 / Uragan-M sn 742. Mass: 1,415 kg (3,119 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 37829 . COSPAR: 2011-055A. Apogee: 19,156 km (11,902 mi). Perigee: 19,104 km (11,870 mi). Inclination: 64.80 deg. Period: 675.70 min. Glonass-M navigation satellite. The Fregat upper stage maneuvered from a 60 km x 220 km orbit on release from the Soyuz third stage; then to 220 km x 220 km, 250 km x 19,100 km and then to the deployment orbit of 19,235 km x 19,667 km x 64.8 deg.. 2011 November 28 - . 08:26 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2478 - . Payload: Glonass-M No. 46. Mass: 1,415 kg (3,119 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 37938 . COSPAR: 2011-071A. Apogee: 19,157 km (11,903 mi). Perigee: 19,102 km (11,869 mi). Inclination: 64.80 deg. Period: 675.70 min. 2011 December 23 - . 12:08 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. FAILURE: Third stage shut down at 7:01 after launch. Stage and payload crashed in Siberia.. Meridian - . Mass: 2,000 kg (4,400 lb). Nation: Russia. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. Was to have been fifth launch of Meridian military communications satellite.. 2013 April 26 - . 05:23 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2485 - . Payload: Glonass-M No. 47. Mass: 1,415 kg (3,119 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 39155 . COSPAR: 2013-019A. Apogee: 19,176 km (11,915 mi). Perigee: 19,084 km (11,858 mi). Inclination: 64.76 deg. Period: 675.73 min. Part of launch series to bring Glonass navigation satellite constellation up to full operation.. 2013 June 7 - . 18:37 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43. Launch Pad: LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2486 - . Mass: 7,100 kg (15,600 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Persona. USAF Sat Cat: 39177 . COSPAR: 2013-028A. Apogee: 733 km (455 mi). Perigee: 714 km (443 mi). Inclination: 98.30 deg. Period: 99.26 min. Second Persona reconnaisance satellite, in sun-synchronous orbit with 10:31 local time descending node. Said to have failed after a short time in orbit.. 2013 June 25 - . 17:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. Launch Pad: LC31/6. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Resurs-P - . Mass: 6,600 kg (14,500 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Yantar. Spacecraft: Resurs-Spektr. USAF Sat Cat: 39186 . COSPAR: 2013-030A. Apogee: 473 km (293 mi). Perigee: 459 km (285 mi). Inclination: 97.28 deg. Period: 93.91 min. Civilian imaging satellite with a Geoton-L1 telescope with 1-meter resolution multispectral imager and a 25m resolution hyperspectral imager.. 2014 March 23 - . 22:54 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2494 - . Payload: Glonass-M No. 54. Mass: 1,415 kg (3,119 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 39620 . COSPAR: 2014-012A. Apogee: 19,174 km (11,914 mi). Perigee: 19,085 km (11,858 mi). Inclination: 64.84 deg. Period: 675.73 min. Glonass-M No. 54 (Uragan-M No. 754) navigation satellite. Incorrectly announced as Cosmos 2491 at time of launch due to confusion in designations applied to three previous classified military launches.. 2014 June 14 - . 17:16 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2500 - . Payload: Glonass-M No. 55. Mass: 1,415 kg (3,119 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 40001 . COSPAR: 2014-032A. Apogee: 19,262 km (11,968 mi). Perigee: 19,145 km (11,896 mi). Inclination: 64.78 deg. Period: 678.67 min. Glonass-M satellite No. 55 to supplement the Russian navigation satellite constellation.. 2014 July 8 - . 15:58 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Meteor M2 - . Mass: 2,700 kg (5,900 lb). Nation: Russia. Spacecraft: Meteor. USAF Sat Cat: 40069 . COSPAR: 2014-037A. Apogee: 827 km (513 mi). Perigee: 820 km (500 mi). Inclination: 98.80 deg. Period: 101.37 min. Second in series of replacements for Meteor-M weather satellites.. MKA PN2 (Relek) - . Mass: 250 kg (550 lb). Nation: Russia. Spacecraft Bus: Karat. Spacecraft: Relek. USAF Sat Cat: 40070 . COSPAR: 2014-037B. Apogee: 821 km (510 mi). Perigee: 622 km (386 mi). Inclination: 98.38 deg. Period: 99.22 min. Carried magnetosphere instruments.. DX 1 - . Mass: 27 kg (59 lb). Nation: Russia. Spacecraft: DX 1. USAF Sat Cat: 40071 . COSPAR: 2014-037C. Apogee: 638 km (396 mi). Perigee: 624 km (387 mi). Inclination: 98.40 deg. Period: 97.33 min. Experimental small satellite bus; carried an Automatic Identification System (AIS) receiver for tracking ships.. Skysat 2 - . Mass: 100 kg (220 lb). Nation: USA. Spacecraft: Skysat. USAF Sat Cat: 40072 . COSPAR: 2014-037D. Apogee: 635 km (394 mi). Perigee: 624 km (387 mi). Inclination: 98.40 deg. Period: 97.31 min. Commercial earth optical surveillance satellite by Skybox.. Dummy sat - . Nation: Russia. USAF Sat Cat: 40073 . COSPAR: 2014-037E. Apogee: 634 km (393 mi). Perigee: 624 km (387 mi). Inclination: 98.40 deg. Period: 97.29 min. Ukube 1 - . Mass: 3.00 kg (6.60 lb). Nation: UK. Spacecraft: Cubesat. USAF Sat Cat: 40074 . COSPAR: 2014-037F. Apogee: 633 km (393 mi). Perigee: 623 km (387 mi). Inclination: 98.40 deg. Period: 97.27 min. 3U cubesat sponsored by the UK Space Agency; first of a series to be launched annually to promote space technology in the UK.. Aissat 2 - . Mass: 6.00 kg (13.20 lb). Nation: Norway. Spacecraft: Toronto GNB. USAF Sat Cat: 40075 . COSPAR: 2014-037G. Apogee: 633 km (393 mi). Perigee: 623 km (387 mi). Inclination: 98.40 deg. Period: 97.27 min. Satellite-based Automatic Identification System (AIS) payload to track maritime assets worldwide (all vessels over 300 metric tons are equipped with AIS transponders).. TDS 1 - . Mass: 150 kg (330 lb). Nation: UK. Spacecraft: SSTL-150. USAF Sat Cat: 40076 . COSPAR: 2014-037H. Apogee: 633 km (393 mi). Perigee: 623 km (387 mi). Inclination: 98.39 deg. Period: 97.27 min. TechDemoSat-1 by Surrey Satellite Technology carrying technology payloads from various UK universities.. 2014 November 30 - . 21:52 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2501 - . Payload: Glonass-K1 No. 12L. Mass: 935 kg (2,061 lb). Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Ekspress-1000. USAF Sat Cat: 40315 . COSPAR: 2014-075A. Apogee: 19,179 km (11,917 mi). Perigee: 19,081 km (11,856 mi). Inclination: 64.71 deg. Period: 675.73 min. Second Glonass-K satellite, vehicle No. 12. The Glonass-K series are the third generation of Russian high orbit navigation satellites, following the original Uragan/Glonass and their successors, the Uragan-M/Glonass-M vehicles.. 2014 December 25 - . 03:01 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2502 - . Payload: Lotos-S No. 802. Mass: 6,000 kg (13,200 lb). Nation: Russia. Class: Surveillance. Type: SIGINT. Spacecraft: Lotos-S. USAF Sat Cat: 40358 . COSPAR: 2014-086A. Apogee: 910 km (560 mi). Perigee: 901 km (559 mi). Inclination: 67.15 deg. Period: 103.10 min. Russian military satellite that initially entered a 240 km x 899 km x 67.1 deg orbit. Russian press reports and official announcements did not give any name for the satellite, not even a Cosmos cover name, the first time this had happened since 1963. Believed to be the second Lotos-S signals intelligence satellite. The Lotos-S satellites had a payload similar to the Tselina-2, but used a Russian Yantar-type spacecraft bus from TsSKB-Progress instead of the Tselina-2's Okean class bus from the Ukranian Yuzhnoye organization. The spacecraft circularized its orbit to 899 km x 909 km on December 26, joining Lotos-S No. 801 which was in a 903 km x 907 km x 67 deg orbit. 2014 December 26 - . 18:55 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. Launch Pad: Baikonur LC31/6. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Resurs-P No. 2 - . Mass: 6,600 kg (14,500 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Yantar. Spacecraft: Resurs-Spektr. USAF Sat Cat: 40360 . COSPAR: 2014-087A. Apogee: 475 km (295 mi). Perigee: 463 km (287 mi). Inclination: 97.29 deg. Period: 93.98 min. Resurs-P 47KS No. 2 civil imaging spacecraft. The main payload was the Geoton-L1 imager with 0.5m aperture and 38 km swath, 1.0 m panchromatic and 3 to 4m color resolution. Geoton-L1 had 7 passbands and a 216-channel hyperspectral imager. The KShMSA wide field multispectral camera was also part of the Resurs-P primary payload; an AIS ship tracking receiver from OAO RKS and Lomonosov Federal State Univ.'s Nuklon cosmic ray detector were secondary payloads. Nuklon detected cosmic ray nuclei with atomic number 1 to 30 in the 1 to 1000 TeV energy range. Resurs-P went into a 190 km x 428 km initial orbit that was raised to its operational height of 330 km x 471 km on December 29. Sun synchronous orbit; 1150 GMT local time of the descending node. 2015 June 23 - . 16:44 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2506 - . Mass: 7,000 kg (15,400 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Persona. USAF Sat Cat: 40699 . COSPAR: 2015-029A. Apogee: 725 km (450 mi). Perigee: 706 km (438 mi). Inclination: 98.29 deg. Period: 99.09 min. Third Persona-1 spy satellite, built by TsSKB-Progress in Samara and equipped with electro-optical imaging cameras. Said to be the first to return its data via an optical communications link to an unidentified geosynchronous satellite. On June 28 the satellite manuevered from an elliptical transfer orbit to a circular sun synchronous orbit with 0840 GMT local time of the descending node. 2015 November 17 - . 06:34 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2510 - . Nation: Russia. Class: Surveillance. Type: Early warning satellite. Spacecraft Bus: USP (Victoria). Spacecraft: Tundra. USAF Sat Cat: 41032 . COSPAR: 2015-066A. Apogee: 38,551 km (23,954 mi). Perigee: 1,625 km (1,009 mi). Inclination: 63.80 deg. The first EKS early warning satellite, launched into a Molniya orbit. The satellite, developed by Energiya and Kometa, replaced the defunct Lavochkin/Kometa 'Oko' system.. 2016 February 7 - . 00:21 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2514 - . Payload: Glonass-M No. 51. Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 41330 . COSPAR: 2016-008A. Apogee: 19,158 km (11,904 mi). Perigee: 19,132 km (11,888 mi). Inclination: 64.80 deg. Glonass-M No. 51 (Uragan-M 751, Kosmos-2514) was launched to supplement the Russian navigation constellation.. 2016 March 13 - . 18:56 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Resurs-P No. 3 - . Mass: 6,600 kg (14,500 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Yantar. Spacecraft: Resurs-Spektr. USAF Sat Cat: 41386 . COSPAR: 2016-016A. Apogee: 452 km (280 mi). Perigee: 279 km (173 mi). Inclination: 97.30 deg. Third Resurs-P civil remote sensing satellite. The first two satellites in the series were still operating; Resurs-P No. 1 made an orbit adjust burn on Feb 22. The Resurs-P No. 3 spacecraft, however, failed to deploy one of its solar panels.. 2016 May 29 - . 08:44 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2516 - . Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 41554 . COSPAR: 2016-032A. Apogee: 19,152 km (11,900 mi). Perigee: 19,124 km (11,883 mi). Inclination: 64.80 deg. Glonass-M No. 53 to replenish the Russian navigation satellite system. 2017 May 25 - . 06:32 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2518 - . Payload: EKS No. 2L. Nation: Russia. Spacecraft: Tundra. USAF Sat Cat: 42719 . COSPAR: 2017-027A. Apogee: 38,092 km (23,669 mi). Perigee: 2,267 km (1,408 mi). Inclination: 63.37 deg. Period: 717.86 min. See Kosmos 2518 (Tundra #2, EKS #2). Second Tundra EKS missile early warning satellite.. 2017 September 22 - . 00:02 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2522 - . Payload: Uragan-M No. 752. Nation: Russia. Spacecraft: Glonass. USAF Sat Cat: 42939 . COSPAR: 2017-055A. Apogee: 19,147 km (11,897 mi). Perigee: 19,113 km (11,876 mi). Inclination: 64.56 deg. Period: 675.73 min. See Kosmos 2522 (Uragan-M #46, GLONASS-M №752). .. 2017 November 28 - . 05:40 GMT - . Launch Site: Vostochniy. Launch Complex: Vostochniy PU1S. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Meteor-M No. 2-1 - . Nation: Russia. COSPAR: 2017-F05. See Meteor-M 2-1. .. Lemur-2-BenYeoh - . Payload: Lemur-2-59. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 59 (Lemur-2 BenYeoh). .. Lemur-2-Craig - . Payload: Lemur-2-67. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 67 (Lemur-2 Craig). .. Lemur-2-Ector - . Payload: Lemur-2-66. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 66 (Lemur-2 Ector). .. Lemur-2-CylonRaider - . Payload: Lemur-2-65. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 65 (Lemur-2 CylonRaider). .. Lemur-2-NRE-Metts - . Payload: Lemur-2-64. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 64 (Lemur-2 NRE-Metts). .. Lemur-2-SMillie-Face - . Payload: Lemur-2-63. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 63 (Lemur-2 Smillie-Face). .. Lemur-2-MaxiMillie - . Payload: Lemur-2-62. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 62 (Lemur-2 Maximillie). .. Lemur-2-Matthew - . Payload: Lemur-2-61. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 61 (Lemur-2 Matthew). .. Lemur-2-Harvey - . Payload: Lemur-2-60. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 60 (Lemur-2 Harvey). .. D-Star One - . Nation: Germany. COSPAR: 2017-F05. See D-Star One. .. Landmapper-BC 4 - . Payload: Corvus-BC 4. Nation: USA. COSPAR: 2017-F05. See Landmapper-BC 4 (Corvus-BC 4). .. SEAM - . COSPAR: 2017-F05. See SEAM. .. Landmapper-BC 3 - . Payload: Corvus-BC 3. Nation: USA. COSPAR: 2017-F05. See Landmapper-BC 3 (Corvus-BC 3). .. LEO Vantage 2 - . Nation: USA. COSPAR: 2017-F05. See LEO Vantage 2. .. Baumanets-2 - . COSPAR: 2017-F05. See Baumanets 2. .. IDEA-OSG 1 - . COSPAR: 2017-F05. See IDEA-OSG 1. .. AISSAT-3 - . Nation: Norway. COSPAR: 2017-F05. See AISSat 3. .. Lemur-2-McGarvey - . Payload: Lemur-2-58. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-F05. See Lemur-2 60 (Lemur-2 Harvey). .. 2017 December 2 - . 10:42 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2524 - . Payload: Lotos-S1 No. 803. Nation: Russia. Spacecraft: Lotos-S. USAF Sat Cat: 43032 . COSPAR: 2017-076A. Apogee: 910 km (560 mi). Perigee: 900 km (550 mi). Inclination: 67.15 deg. Period: 103.10 min. See Kosmos 2524 (Lotos-S1 #2). .. 2018 March 9 - . 17:09 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELS. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. O3b FM15 - . Payload: O3b 15. Nation: USA. USAF Sat Cat: 43231 . COSPAR: 2018-024A. Apogee: 8,070 km (5,010 mi). Perigee: 8,062 km (5,009 mi). Inclination: 0.0400 deg. Period: 287.93 min. See O3b FM15. .. Additional Details: here.... O3b FM16 - . Payload: O3b 16. Nation: USA. USAF Sat Cat: 43232 . COSPAR: 2018-024B. Apogee: 8,070 km (5,010 mi). Perigee: 8,061 km (5,008 mi). Inclination: 0.0300 deg. Period: 287.93 min. See O3b FM16. .. O3b FM14 - . Payload: O3b 14. Nation: USA. USAF Sat Cat: 43233 . COSPAR: 2018-024C. Apogee: 8,070 km (5,010 mi). Perigee: 8,061 km (5,008 mi). Inclination: 0.0300 deg. Period: 287.93 min. See O3b FM14. .. Additional Details: here.... O3b FM13 - . Payload: O3b 13. Nation: USA. USAF Sat Cat: 43234 . COSPAR: 2018-024D. Apogee: 8,073 km (5,016 mi). Perigee: 8,059 km (5,007 mi). Inclination: 0.0300 deg. Period: 287.93 min. See O3b FM13. .. 2018 June 16 - . 21:45 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2527 - . Payload: Uragan-M No. 756. Nation: Russia. Spacecraft: Glonass. USAF Sat Cat: 43508 . COSPAR: 2018-053A. Apogee: 19,145 km (11,896 mi). Perigee: 19,115 km (11,877 mi). Inclination: 64.83 deg. Period: 675.73 min. See Kosmos 2527 (Uragan-M #47, GLONASS-M №756). .. 2018 October 25 - . 00:14 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2528 - . Payload: Lotos-S1 No. 804. Nation: Russia. Spacecraft: Lotos-S. USAF Sat Cat: 43657 . COSPAR: 2018-082A. Apogee: 910 km (560 mi). Perigee: 901 km (559 mi). Inclination: 67.15 deg. Period: 103.10 min. See Kosmos 2528 (Lotos-S1 #3). .. 2018 November 3 - . 20:16 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1B. Cosmos 2529 - . Payload: Uragan-M No. 757. Nation: Russia. Spacecraft: Glonass. USAF Sat Cat: 43687 . COSPAR: 2018-086A. Apogee: 19,155 km (11,902 mi). Perigee: 19,105 km (11,871 mi). Inclination: 64.77 deg. Period: 675.73 min. See Kosmos 2529 (Uragan-M #48, GLONASS-M №757). .. 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