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Dombarovskiy
Headquarters of an RVSN Division, 1964-present. Operated 64 heavy ICBM silos (R-36/R-36M). Two silos were modified to launch surplus R-36M missiles as orbital launch vehicles.

AKA: Yasniy. First Launch: 1968-03-01. Last Launch: 2014-06-19. Number: 99 . Location: Orenburg. Longitude: 59.8500 deg. Latitude: 51.2071 deg.



Subtopics

Dombarovskiy Sh370/13 Null

Family: ICBM Base. Country: Russia. Spacecraft: ChubuSat, Hodoyoshi, NEXTAR NX-300L, Tsubame, Tsukushi, ROCSAT, Genesis Pathfinder. Launch Vehicles: R-36M2 15A18M, Dnepr. Agency: RVSN.

1968 Mar - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 Jul - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974? - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 Jul - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 Jul - . Launch Site: Dombarovskiy. Launch Vehicle: UR-100.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1975? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976? - . Launch Site: Dombarovskiy. LV Family: R-16. Launch Vehicle: R-16U.
  • Nation: Russia. Agency: RVSN. Apogee: 1,210 km (750 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978? - . Launch Site: Dombarovskiy. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2004 December 22 - . 08:30 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: R-36M2 15A18M.
  • R-36M2 ICBM demonstration flight - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

    The sixteen-year old missile was launched from an operational ICBM base and its dummy warheads impacted in the test range on the Kamchatka Peninsula after a 6,000 kilometer flight. The test was touted as a demonstration of use of the surplus ICBM's, launched directly from their silos, for launch of commerical orbital payloads, in lieu of more expensive decommissioning. Others saw it as the beginning of the development of Dombarovskiy into a new spaceport, on Russian soil, in replacement of Baikonur.


2006 July 12 - . 14:53 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Genesis 1 - . Mass: 1,360 kg (2,990 lb). Nation: USA. Agency: RVSN. Manufacturer: Bigelow. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Bigelow. Spacecraft: Genesis Pathfinder. USAF Sat Cat: 29252 . COSPAR: 2006-029A. Apogee: 565 km (351 mi). Perigee: 552 km (342 mi). Inclination: 64.5000 deg. Period: 95.80 min. One third scale version of the privately-financed Nautilus inflatable human space habitat module..

2006 December 21 - . 08:20 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: R-36M2 15A18M.
  • OT - . Nation: Russia. Apogee: 1,000 km (600 mi).

2007 June 28 - . 15:02 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Genesis 2 - . Mass: 1,360 kg (2,990 lb). Nation: USA. Agency: Makeyev bureau. Manufacturer: Bigelow. Class: Manned. Type: Manned space station. Spacecraft Bus: Bigelow. Spacecraft: Genesis Pathfinder. USAF Sat Cat: 31789 . COSPAR: 2007-028A. Apogee: 561 km (348 mi). Perigee: 556 km (345 mi). Inclination: 64.5000 deg. Period: 95.80 min.

    One third scale version of the privately-financed Nautilus inflatable human space habitat module. The spacecraft's 22 interior and exterior cameras provided images of items and pictures carried for paying participants in Bigelow's “Fly your Stuff” program.


2008 October 1 - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Theos - . Mass: 715 kg (1,576 lb). Nation: Thailand. Agency: Makeyev bureau. Manufacturer: EADS Astrium. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft Bus: T200. Spacecraft: ROCSAT. USAF Sat Cat: 33396 . COSPAR: 2008-049A. Apogee: 693 km (430 mi). Perigee: 673 km (418 mi). Inclination: 98.8000 deg. Period: 98.40 min. Thai surveillance satellite, based on EADS Astrium bus used for ROCSAT-2..

2009 December 24 - . 06:30 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: R-36M2 15A18M.
  • RV x 10? - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Test.

2010 June 15 - . 14:42 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Picard - . Mass: 100 kg (220 lb). Nation: France. Agency: Makeyev bureau. Class: Astronomy. Type: Solar satellite. Spacecraft: Myriade. USAF Sat Cat: 36598 . COSPAR: 2010-028A. Apogee: 730 km (450 mi). Perigee: 725 km (450 mi). Inclination: 98.3000 deg. Period: 99.30 min. Solar observation payload..
  • Prisma - . Mass: 140 kg (300 lb). Nation: Sweden. Agency: Makeyev bureau. Class: Technology. Type: Technology satellite. Spacecraft: Prisma. USAF Sat Cat: 36599 . COSPAR: 2010-028B. Apogee: 787 km (489 mi). Perigee: 724 km (449 mi). Inclination: 98.3000 deg. Period: 99.90 min. Prototype Research Instruments and Space Mission technology Advancement satellite to test space rendezvous and formation-flight technologies. Consisted of 140 kg primary satellite and 40 kg target..

2011 August 17 - . 07:12 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • RASAT - . Mass: 95 kg (209 lb). Nation: Turkey. Class: Earth. Type: Earth resources satellite. Spacecraft: RASAT. USAF Sat Cat: 37791 . COSPAR: 2011-044D. Apogee: 699 km (434 mi). Perigee: 666 km (413 mi). Inclination: 98.2000 deg. Period: 98.40 min. Turkish Earth observation satellite with a Korean-built imager, built for TUBITAK, the Turkish science research council and UZAY, the Space Technology Research Insitute in Ankara..
  • Aprizesat 5 - . Mass: 14 kg (30 lb). Nation: USA. Program: AIS. Class: Communications. Type: Communications satellite. Spacecraft: Aprizesat. USAF Sat Cat: 37792 . COSPAR: 2011-044E. Apogee: 697 km (433 mi). Perigee: 610 km (370 mi). Inclination: 98.3000 deg. Period: 97.80 min.

    Aprizesat 5 and 6 were built by SpaceQuest for exactEarth Ltd. Equipped with AIS (maritime Automatic Identification System) payloads for ship location tracking. The exactEarth system also included the SpaceQuest AprizeSat 3 and 4, and a payload attached to ISRO's ResourceSat-2 satellite.

  • Aprizesat 6 - . Mass: 14 kg (30 lb). Nation: USA. Program: AIS. Class: Communications. Type: Communications satellite. Spacecraft: Aprizesat. USAF Sat Cat: 37793 . COSPAR: 2011-044F. Apogee: 698 km (433 mi). Perigee: 627 km (389 mi). Inclination: 98.3000 deg. Period: 98.00 min. Part of a constellation of small LEO satellites for global fixed and mobile asset tracking. Also carried an AIS (Automatic Identification System) receiver monitor naval vessel locations..
  • Sich 2 - . Mass: 175 kg (385 lb). Nation: Ukraine. Class: Earth. Type: Earth resources satellite. Spacecraft: Sich. USAF Sat Cat: 37794 . COSPAR: 2011-044G. Apogee: 703 km (436 mi). Perigee: 684 km (425 mi). Inclination: 98.2000 deg. Period: 98.60 min. Ukrainian remote sensing satellite built by Yuzhnoye..
  • BPA-2/SL-24 - . Nation: Russia. Class: Technology. Type: Technology satellite. USAF Sat Cat: 37795 . COSPAR: 2011-044H. Apogee: 1,296 km (805 mi). Perigee: 692 km (429 mi). Inclination: 98.2000 deg. Period: 105.00 min.

    Yuzhnoye launch vehicle engineering payload which remained attached to the post-boost maneuvering upper stage after deployment of the other six satellites on the launch. 16 minutes after launch, at an altitude of 700 km, the upper stage dispensed the six satellites at two-minute intervals, then maneuvered into itself into a higher orbit.


2013 August 22 - . 14:39 GMT - . Launch Site: Dombarovskiy. Launch Pad: Yasniy Sh370/13. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Arirang-5 - . Payload: Kompsat-5. Mass: 1,400 kg (3,000 lb). Nation: Korea South. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: T200. Spacecraft: Kompsat. USAF Sat Cat: 39227 . COSPAR: 2013-042A. Apogee: 560 km (340 mi). Perigee: 545 km (338 mi). Inclination: 97.6000 deg. Period: 95.70 min. South Korea's first X-band SAR satellite..

2013 Sep 27? - . Launch Site: Dombarovskiy. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35.
  • Hypersonic RV - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2013 October 30 - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: R-36M2 15A18M.
  • 10 RVs?? - . Nation: Russia. Apogee: 1,000 km (600 mi). Launched from Dombarovskiy to to Kura. One of a series of missiles launched on the same day as part of a large scale Russian military exercise..

2013 November 21 - . 07:10 GMT - . Launch Site: Dombarovskiy. Launch Pad: xxx. LV Family: R-36M. Launch Vehicle: Dnepr.
  • AprizeSat-7 - . Mass: 14 kg (30 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: AprizeSat. USAF Sat Cat: 39416 . COSPAR: 2013-066A. Apogee: 650 km (400 mi). Perigee: 593 km (368 mi). Inclination: 97.7800 deg. Period: 97.14 min.

    Communications satellites for SpaceQuest; part of a constellation of small LEO satellites for global fixed and mobile asset tracking. Also carried an AIS (Automatic Identification System) receiver monitor naval vessel locations. Dnepr rocket launched from an ICBM silo at Yasniy in Russia placed a cluster of 24 satellites in orbit on on a single launch. Although this was fewer than the ORS-3 launch the day before, if nanosats ejected later are counted, the single launch put 33 payloads in orbit.

  • HINCube-1 - . Mass: 1.00 kg (2.20 lb). Nation: South Africa. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39417 . COSPAR: 2013-066B. Apogee: 678 km (421 mi). Perigee: 592 km (367 mi). Inclination: 97.7800 deg. Period: 97.42 min. 1U cubesat from French South African Institute of Technology at the Cape Peninsula University of Technology. Mission: Space weather, technology demonstration, education and human capital development.. Successful. First South African CubeSat..
  • SkySat-1 - . Mass: 90 kg (198 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Skysat. USAF Sat Cat: 39418 . COSPAR: 2013-066C. Apogee: 595 km (369 mi). Perigee: 564 km (350 mi). Inclination: 97.7900 deg. Period: 96.26 min. Imaging satellite, the first for the US company Skybox..
  • Dubaisat-2 - . Mass: 300 kg (660 lb). Nation: UAE. Class: Surveillance. Type: Surveillance satellite. Spacecraft: SI-300. USAF Sat Cat: 39419 . COSPAR: 2013-066D. Apogee: 600 km (370 mi). Perigee: 583 km (362 mi). Inclination: 97.7900 deg. Period: 96.51 min. Imaging satellite for the United Arab Emirates build by Satrec of South Korea..
  • OPTOS - . Mass: 4.00 kg (8.80 lb). Nation: Spain. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39420 . COSPAR: 2013-066E. Apogee: 793 km (492 mi). Perigee: 594 km (369 mi). Inclination: 97.7600 deg. Period: 98.63 min. 3U cubesat from INTA of Spain..
  • Unisat-5 - . Mass: 19 kg (41 lb). Nation: Italy. Class: Technology. Type: Technology satellite. Spacecraft: Unisat. USAF Sat Cat: 39421 . COSPAR: 2013-066F. Apogee: 636 km (395 mi). Perigee: 592 km (367 mi). Inclination: 97.7800 deg. Period: 96.97 min.

    Technology satellite for the University of Rome. It carried a further eight tiny satellites within it, and one of those (PUCP-Sat) carried a further nested satellite, Pocket-PUCP. Most of the subsatellites were ejected from Unisat-5 between 08:10 and 08:25 GMT on November 21.

  • STSat-3 - . Mass: 170 kg (370 lb). Nation: Korea South. Class: Astronomy. Type: Astronomy satellite. Spacecraft: STSat. USAF Sat Cat: 39422 . COSPAR: 2013-066G. Apogee: 622 km (386 mi). Perigee: 591 km (367 mi). Inclination: 97.7800 deg. Period: 96.83 min.

    Satellite built by KAIST of South Korea, with the MIRIS infrared astronomy experiment (an 8 cm telescope operating at 0.9-2 microns with a 4 degree field of view for spectroscopy of diffuse extended emission), as well as earth imaging and technology payloads.

  • WNISAT-1 - . Mass: 10 kg (22 lb). Nation: Japan. Class: Earth. Type: Weather satellite. Spacecraft: WNISAT. USAF Sat Cat: 39423 . COSPAR: 2013-066H. Apogee: 845 km (525 mi). Perigee: 594 km (369 mi). Inclination: 97.7500 deg. Period: 99.19 min. 30 cm cube for Weather News Inc. and Axelspace, to monitor northern sea routes and atmospheric CO2..
  • KHUSAT-1 - . Payload: CINEMA 2. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 39424 . COSPAR: 2013-066J. Apogee: 727 km (451 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.94 min. 3U cubesat from Kyung Hee University, Seoul, to join the CINEMA constellation..
  • AprizeSat-8 - . Mass: 14 kg (30 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: AprizeSat. USAF Sat Cat: 39425 . COSPAR: 2013-066K. Apogee: 666 km (413 mi). Perigee: 593 km (368 mi). Inclination: 97.7800 deg. Period: 97.31 min. Part of a constellation of small LEO satellites for global fixed and mobile asset tracking. Also carried an AIS (Automatic Identification System) receiver monitor naval vessel locations..
  • KHUSAT-2 - . Payload: CINEMA 3. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 39426 . COSPAR: 2013-066L. Apogee: 743 km (461 mi). Perigee: 594 km (369 mi). Inclination: 97.7700 deg. Period: 98.11 min. 3U cubesat from Kyung Hee University, Seoul, to join the CINEMA constellation..
  • Triton 1 - . Mass: 4.00 kg (8.80 lb). Nation: UK. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 39427 . COSPAR: 2013-066M. Apogee: 758 km (470 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.27 min. 3U cubesat test of an AIS receiver from ISIS b.v., Netherlands..
  • Delfi-3nXt - . Mass: 5.00 kg (11.00 lb). Nation: Netherlands. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39428 . COSPAR: 2013-066N. Apogee: 773 km (480 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.41 min. 3U cubesat from Delft University of Technology..
  • Dove-3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 39429 . COSPAR: 2013-066P. Apogee: 809 km (502 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.80 min. 3U imaging satellite from PlanetLabs, San Francisco..
  • GOMX-1 - . Mass: 6.00 kg (13.20 lb). Nation: Denmark. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 39430 . COSPAR: 2013-066Q. Apogee: 813 km (505 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.84 min. 2U cubesat test an ADS-B air traffic control receiver, for GOMSpace, Aalborg, Denmark..
  • Lem - . Payload: BRITE-PL. Mass: 6.00 kg (13.20 lb). Nation: Poland. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 39431 . COSPAR: 2013-066R. Apogee: 884 km (549 mi). Perigee: 594 km (369 mi). Inclination: 97.7500 deg. Period: 99.59 min. Satellite using Toronto's GNB bus carrying the BRITE-PL astronomical photometry payload for the Polish Academy of Sciences..
  • ICUBE-1 - . Mass: 2.00 kg (4.40 lb). Nation: Pakistan. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39432 . COSPAR: 2013-066S. Apogee: 634 km (393 mi). Perigee: 587 km (364 mi). Inclination: 97.7800 deg. Period: 96.90 min. 2U cubesat from Unisat-5 for Institute of Space Technology, Islamabad. Successful. First Pakistani cubesat..
  • HUMSAT-D - . Mass: 1.00 kg (2.20 lb). Nation: Spain. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39433 . COSPAR: 2013-066T. Apogee: 632 km (392 mi). Perigee: 586 km (364 mi). Inclination: 97.7800 deg. Period: 96.88 min. Deployed from Unisat-5 for University of Vigo, Spain..
  • Dove-4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 39434 . COSPAR: 2013-066U. Apogee: 624 km (387 mi). Perigee: 581 km (361 mi). Inclination: 97.7800 deg. Period: 96.75 min. 3U Earth imaging satellite, deployed from Unisat-5 for PlanetLabs..
  • WREN - . Mass: 0 kg (0 lb). Nation: Germany. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39435 . COSPAR: 2013-066V. Apogee: 638 km (396 mi). Perigee: 594 km (369 mi). Inclination: 97.8000 deg. Period: 97.02 min. PocketQube cubesat from StaDoKo (spinoff company of the University of Aachen)..
  • 50SAT - . Mass: 0 kg (0 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39436 . COSPAR: 2013-066W. Apogee: 615 km (382 mi). Perigee: 580 km (360 mi). Inclination: 97.7800 deg. Period: 96.63 min. AKA Eagle-2, 50DollarSat; from Morehead State University. First PocketQube cubesat; 1P size was 0.15 kg, 5 x 5 x 5cm cubes.
  • BeakerSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39437 . COSPAR: 2013-066X. Apogee: 619 km (384 mi). Perigee: 583 km (362 mi). Inclination: 97.7900 deg. Period: 96.71 min. 2.5P PocketQube, AKA Eagle-1, from Morehead State University..
  • VELOX-P2 - . Mass: 1.00 kg (2.20 lb). Nation: Singapore. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39438 . COSPAR: 2013-066Y. Apogee: 695 km (431 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.60 min. Cubesat from Nanyang Tech University..
  • First-Move - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39439 . COSPAR: 2013-066Z. Apogee: 691 km (429 mi). Perigee: 591 km (367 mi). Inclination: 97.7700 deg. Period: 97.54 min. Cubesat from Technical University of Munich..
  • Manolito - . Payload: CUBEBUG 2. Mass: 2.00 kg (4.40 lb). Nation: Argentina. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39440 . COSPAR: 2013-066AA. Apogee: 710 km (440 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.76 min. 2U cubesat from Argentina..
  • Krysaor - . Payload: NEE-2. Mass: 1.00 kg (2.20 lb). Nation: Ecuador. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39441 . COSPAR: 2013-066AB. Apogee: 711 km (441 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.77 min. Cubesat from Ecuadorian Space Agency..
  • PUCPSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: Peru. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39442 . COSPAR: 2013-066AC. Apogee: 633 km (393 mi). Perigee: 587 km (364 mi). Inclination: 97.7800 deg. Period: 96.90 min. 1U cubesat deployed from Unisat-5 for Pontifica Universidad Catolica del Peru, Lima..
  • QBScout-1 - . Mass: 0 kg (0 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39443 . COSPAR: 2013-066AD. Apogee: 630 km (390 mi). Perigee: 591 km (367 mi). Inclination: 97.7800 deg. Period: 96.90 min. 2.5P PocketQube from University of Maryland/Baltimore County..
  • FUNcube-1 - . Mass: 1.00 kg (2.20 lb). Nation: UK. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39444 . COSPAR: 2013-066AE. Apogee: 677 km (420 mi). Perigee: 592 km (367 mi). Inclination: 97.7700 deg. Period: 97.41 min. Cubesat for AMSAT-UK..
  • Tshepiso - . Payload: ZACUBE. Mass: 1.00 kg (2.20 lb). Nation: Norway. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39445 . COSPAR: 2013-066AF. Apogee: 677 km (420 mi). Perigee: 592 km (367 mi). Inclination: 97.7700 deg. Period: 97.41 min. Cubesat from South Africa's Cape Peninsula University of Tech (CPUT)..
  • UWE-3 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39446 . COSPAR: 2013-066AG. Apogee: 694 km (431 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.59 min. Cubesat from University of Wurzburg..
  • BPA-3 - . Payload: SL-24. Nation: Russia. Class: Technology. Type: Technology satellite. USAF Sat Cat: 39448 . COSPAR: 2013-066AJ. Apogee: 1,610 km (1,000 mi). Perigee: 591 km (367 mi). Inclination: 97.6700 deg. Period: 107.27 min. Yuzhnoye experiment attached to final stage of rocket..
  • Pocket-PUCP - . Mass: 0 kg (0 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39437 . COSPAR: 2013-066x. Apogee: 616 km (382 mi). Perigee: 579 km (359 mi). Inclination: 97.7800 deg. Period: 96.64 min. PocketQube cubesat ejected from PUCPSat-1..

2014 June 19 - . 19:11 GMT - . Launch Site: Dombarovskiy. Launch Pad: Sh370/13. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Kazeosat 2 - . Mass: 177 kg (390 lb). Nation: Kazakhstan. Spacecraft: SSTL-150. USAF Sat Cat: 40010 . COSPAR: 2014-033A. Apogee: 637 km (395 mi). Perigee: 610 km (370 mi). Inclination: 97.9800 deg. Period: 97.18 min. Kazakh medium resolution imaging satellite; had an imager with 6.5 metre resolution and a 77 km swath width..
  • Hodoyoshi 4 - . Mass: 64 kg (141 lb). Nation: Japan. Spacecraft: Hodoyoshi. USAF Sat Cat: 40011 . COSPAR: 2014-033B. Apogee: 651 km (404 mi). Perigee: 612 km (380 mi). Inclination: 97.9800 deg. Period: 97.34 min. Experimental earth-observation satellite by the University of Toky with a 5 m ground resolution..
  • Unisat 6 - . Mass: 26 kg (57 lb). Nation: Italy. Spacecraft: Unisat. USAF Sat Cat: 40012 . COSPAR: 2014-033C. Apogee: 699 km (434 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.86 min. Satellite by GAUSS Srl to test customer equipment and deploy four cubesats..
  • Deimos 2 - . Mass: 300 kg (660 lb). Nation: Spain. Spacecraft: Deimos 2. USAF Sat Cat: 40013 . COSPAR: 2014-033D. Apogee: 622 km (386 mi). Perigee: 597 km (370 mi). Inclination: 97.9700 deg. Period: 96.88 min. Earth observation satellite which carried an 0.75m resolution, 12 km swath imager provided by Satrec South Korea. Total cost including launch was 60 million Euros..
  • Bugsat 1 - . Mass: 22 kg (48 lb). Nation: Argentina. Spacecraft: Bugsat. USAF Sat Cat: 40014 . COSPAR: 2014-033E. Apogee: 618 km (384 mi). Perigee: 568 km (352 mi). Inclination: 97.9900 deg. Period: 96.54 min. Technology testbed for components for a planned constellation of earth observation satellites by Satellogic SA..
  • Hodoyoshi 3 - . Mass: 58 kg (127 lb). Nation: Japan. Spacecraft: Hodoyoshi. USAF Sat Cat: 40015 . COSPAR: 2014-033F. Apogee: 666 km (413 mi). Perigee: 612 km (380 mi). Inclination: 97.9700 deg. Period: 97.50 min. Experimental earth-observation satellite by the University of Toky with a 40 m ground resolution..
  • Saudisat 4 - . Mass: 100 kg (220 lb). Nation: Saudi Arabia. Spacecraft Bus: Saudisat. Spacecraft: Saudisat 4. USAF Sat Cat: 40016 . COSPAR: 2014-033G. Apogee: 682 km (423 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.67 min. Technology demonstration satellite King Abdulaziz City for Science and Technology with a joint NASA Ames payload related to gravitational reference sensors for drag-free spacecraft..
  • Tabletsat Aurora - . Mass: 25 kg (55 lb). Nation: Russia. Spacecraft: Tabletsat Aurora. USAF Sat Cat: 40017 . COSPAR: 2014-033H. Apogee: 619 km (384 mi). Perigee: 581 km (361 mi). Inclination: 97.9800 deg. Period: 96.69 min. Technology demonstrator with an imaging payload by SPUTNIX with a panchromatic ground resolution of 15 m and 47 km swath width..
  • Aprizesat 9 - . Mass: 14 kg (30 lb). Nation: USA. Spacecraft: AprizeSat. USAF Sat Cat: 40018 . COSPAR: 2014-033J. Apogee: 715 km (444 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 98.02 min. Part of a constellation of small LEO satellites for global fixed and mobile asset tracking. Also carried an AIS (Automatic Identification System) receiver monitor naval vessel locations..
  • Aprizesat 10 - . Mass: 14 kg (30 lb). Nation: USA. Spacecraft: AprizeSat. USAF Sat Cat: 40019 . COSPAR: 2014-033K. Apogee: 733 km (455 mi). Perigee: 613 km (380 mi). Inclination: 97.9600 deg. Period: 98.21 min. Part of a constellation of small LEO satellites for global fixed and mobile asset tracking. Also carried an AIS (Automatic Identification System) receiver monitor naval vessel locations..
  • Brite Toronto - . Mass: 10 kg (22 lb). Nation: Canada. Spacecraft: Toronto GNB. USAF Sat Cat: 40020 . COSPAR: 2014-033L. Apogee: 739 km (459 mi). Perigee: 613 km (380 mi). Inclination: 97.9600 deg. Period: 98.27 min. BRIght-star Target Explorer to observe the brightest starts for variability..
  • Duchifat 1 - . Mass: 1.00 kg (2.20 lb). Nation: Israel. Spacecraft: Cubesat. USAF Sat Cat: 40021 . COSPAR: 2014-033M. Apogee: 623 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9700 deg. Period: 96.94 min. 1U cubesat by the Herzliya Science Center..
  • Pace - . Mass: 3.00 kg (6.60 lb). Nation: Taiwan. Spacecraft: Cubesat. USAF Sat Cat: 40022 . COSPAR: 2014-033N. Apogee: 623 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.94 min. 2U cubesat for the National Cheng Kung University..
  • Flock 1C 10 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40023 . COSPAR: 2014-033P. Apogee: 623 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.94 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Nanosat C BR1 - . Mass: 1.00 kg (2.20 lb). Nation: Brazil. Spacecraft: Cubesat. USAF Sat Cat: 40024 . COSPAR: 2014-033Q. Apogee: 623 km (387 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.94 min. 1U cubesat for the Southern Regional Space Research Center..
  • Qb50P1 - . Mass: 2.00 kg (4.40 lb). Nation: Belgium. Spacecraft: Cubesat. USAF Sat Cat: 40025 . COSPAR: 2014-033R. Apogee: 623 km (387 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.95 min. 2U cubesat; part of a constellation of 50 CubeSats built by university teams to study the llower thermosphere..
  • Flock 1C 7 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40026 . COSPAR: 2014-033S. Apogee: 622 km (386 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.94 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1C 1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40027 . COSPAR: 2014-033T. Apogee: 623 km (387 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.95 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Popsat Hip 1 - . Mass: 3.00 kg (6.60 lb). Nation: Singapore. Spacecraft: Cubesat. USAF Sat Cat: 40028 . COSPAR: 2014-033U. Apogee: 625 km (388 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.96 min. 3U cubesat by Microspace Rapid..
  • Flock 1C 2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40029 . COSPAR: 2014-033V. Apogee: 625 km (388 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Dtusat 2 - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Spacecraft: Cubesat. USAF Sat Cat: 40030 . COSPAR: 2014-033W. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9700 deg. Period: 96.97 min. 1U cubesat by the Danish Technical University..
  • Flock 1C 4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40031 . COSPAR: 2014-033X. Apogee: 624 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.95 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Qb50p2 - . Mass: 2.00 kg (4.40 lb). Nation: Belgium. Spacecraft: Cubesat. USAF Sat Cat: 40032 . COSPAR: 2014-033Y. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 96.97 min. 2U cubesat; part of a constellation of 50 CubeSats built by university teams to study the llower thermosphere..
  • Flock 1C 11 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40033 . COSPAR: 2014-033Z. Apogee: 624 km (387 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Antelsat - . Mass: 3.00 kg (6.60 lb). Nation: Uruguay. Spacecraft: Cubesat. USAF Sat Cat: 40034 . COSPAR: 2014-033AA. Apogee: 700 km (430 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.87 min. 2U cubesat by Uruguayan State Faculty of engineering; carried infrared imager and amateur radio payloads..
  • Flock 1C 9 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40035 . COSPAR: 2014-033AB. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 96.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1C 6 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40036 . COSPAR: 2014-033AC. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 96.98 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Perseus M2 - . Mass: 7.00 kg (15.40 lb). Nation: Russia. Spacecraft: Cubesat. USAF Sat Cat: 40037 . COSPAR: 2014-033AD. Apogee: 626 km (388 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.99 min. 6U Cubesat by by Canopus Systems with an Automatic Identification System (AIS) receiver for tracking shipping..
  • Flock 1C 5 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40038 . COSPAR: 2014-033AE. Apogee: 626 km (388 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.98 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Perseus M1 - . Mass: 7.00 kg (15.40 lb). Nation: Russia. Spacecraft: Cubesat. USAF Sat Cat: 40039 . COSPAR: 2014-033AF. Apogee: 627 km (389 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 97.01 min. 6U Cubesat by by Canopus Systems with an Automatic Identification System (AIS) receiver for tracking shipping..
  • Flock 1C 8 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40040 . COSPAR: 2014-033AG. Apogee: 626 km (388 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.99 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1C 3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40041 . COSPAR: 2014-033AH. Apogee: 625 km (388 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.98 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Polyitan 1 - . Mass: 1.00 kg (2.20 lb). Nation: Ukraine. Spacecraft: Cubesat. USAF Sat Cat: 40042 . COSPAR: 2014-033AJ. Apogee: 628 km (390 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 97.01 min. 1U cubesat by National Technical University of Ukraine..
  • Tigrisat - . Mass: 3.00 kg (6.60 lb). Nation: Iraq. Spacecraft: Cubesat. USAF Sat Cat: 40043 . COSPAR: 2014-033AK. Apogee: 698 km (433 mi). Perigee: 610 km (370 mi). Inclination: 97.9700 deg. Period: 97.81 min. 3U cubesat built by Iraqi students at the La Sapienza University of Rome..
  • Lemur 1 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 40044 . COSPAR: 2014-033AL. Apogee: 697 km (433 mi). Perigee: 611 km (379 mi). Inclination: 97.9700 deg. Period: 97.82 min. 3U cubesat by NanoSatisfi Inc..
  • Aerocube 6a - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 40045 . COSPAR: 2014-033AM. Apogee: 700 km (430 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.87 min.
  • Aerocube 6b - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 40046 . COSPAR: 2014-033AN. Apogee: 700 km (430 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.87 min.

2014 November 6 - . 07:35 GMT - . Launch Site: Dombarovskiy. Launch Complex: Dombarovskiy. Launch Pad: Yasniy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • ASNARO - . Mass: 495 kg (1,091 lb). Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: NEXTAR NX-300L. USAF Sat Cat: 40298 . COSPAR: 2014-070A. Apogee: 509 km (316 mi). Perigee: 506 km (314 mi). Inclination: 97.4500 deg. Period: 94.77 min.

    High resolution imaging satellite developed by NEC and managed by Japan Space Systems (formerly USEF, part of the Ministry of Trade and Industry) rather than by the main Japanese space agency JAXA. The ASNARO had 0.5m resolution on a 10 km nadir swath width. Sun synchronous orbit; 1100 GMT local time of the descending node.

  • Hodoyoshi-1 - . Mass: 50 kg (110 lb). Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Hodoyoshi. USAF Sat Cat: 40299 . COSPAR: 2014-070B. Apogee: 513 km (318 mi). Perigee: 496 km (308 mi). Inclination: 97.4500 deg. Period: 94.70 min. Satellite of the University of Tokyo and AXELSPACE, carried an imager with 6.8m resolution and 28 km swath. Sun synchronous orbit; 1100 GMT local time of the descending node..
  • Kinshachi-1 - . Payload: CHUBUSAT 1. Mass: 50 kg (110 lb). Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: ChubuSat. USAF Sat Cat: 40300 . COSPAR: 2014-070C. Apogee: 524 km (325 mi). Perigee: 496 km (308 mi). Inclination: 97.4400 deg. Period: 94.82 min.

    Also known as also known as ChubuSat-1, a project of Nagoya and Daido universities. (The name Kinschachi refers to the golden sea-monster statues on Nagoya castle). It carries d 10m resolution, 14 km swath imager, a 130 m resolution, 7-13 micron infrared camera reported to be for atmosphere temperature profiles and space debris monitoring, and an amateur radio relay payload. Sun synchronous orbit; 1055 GMT local time of the descending node.

  • Tsukushi - . Payload: QSAT-EOS. Mass: 49 kg (108 lb). Nation: Japan. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Tsukushi. USAF Sat Cat: 40301 . COSPAR: 2014-070D. Apogee: 530 km (320 mi). Perigee: 489 km (303 mi). Inclination: 97.4400 deg. Period: 94.81 min.

    'Horsetail'; also called QSAT-EOS, Kyushu Satellite for Earth Observation System Demonstration. The satellite carried a CMOS camera with 4 m resolution and 7 km swath, a magnetometer and an in-situ space debris detector, as well as a deployable 3-meter kapton sail used as a drag augmentation device. Sun synchronous orbit; 1055 GMT local time of the descending node.

  • Tsubame - . Mass: 49 kg (108 lb). Nation: Japan. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Tsubame. USAF Sat Cat: 40302 . COSPAR: 2014-070E. Apogee: 553 km (343 mi). Perigee: 495 km (307 mi). Inclination: 97.4400 deg. Period: 95.11 min. 'Swallow', an astronomy satellite from the Tokyo Institute of Technology and carried a hard X-ray polarimeter to study the polarization of gamma ray bursts. Sun synchronous orbit; 1055 GMT local time of the descending node..

2015 March 25 - . 22:08 GMT - . Launch Site: Dombarovskiy. Launch Complex: Yasniy Sh370/13. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Arirang-3A - . Payload: KOMPSAT 3A. Mass: 800 kg (1,760 lb). Nation: Korea South. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: T200. Spacecraft: Kompsat. USAF Sat Cat: 40536 . COSPAR: 2015-014A. Apogee: 538 km (334 mi). Perigee: 522 km (324 mi). Inclination: 97.5300 deg. Period: 95.23 min. South Korean imaging satellite with submeter resolution. Sun synchronous orbit; 0130 GMT local time of the descending node..

2016 April 19 - . 06:41 GMT - . Launch Site: Dombarovskiy. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35.
  • Yu-71 No. 3 - . Nation: Russia. Type: Test. Apogee: 1,000 km (600 mi). Test mission. Impacted in Kura?..

2016 October 25 - . 08:58 GMT - . Launch Site: Dombarovskiy. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35.
  • RV - . Nation: Russia. Type: Test. Apogee: 1,000 km (600 mi). Test mission. Impacted in Kura..


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