Encyclopedia Astronautica
February 26


February 26 Chronology


1921 February 26 - .
1928 February 26 - .
1936 February 26 - .
1941 February 26 - .
  • Birth of Dmitri Andreyevich Yuyukov - . Nation: Russia. Summary: Russian engineer cosmonaut, 1973-1987. Graduated from MAI, 1965 Civilian Engineer, Chelomei OKB. Trained for a TKS flight to the Almaz military space station. Sector Head, NPO Mashinostroyeniye. From worked at GKNPTs Khrunishchev..

1944 February 26 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2.
1945 February 26 - . 16:27 GMT - . Launch Site: V-2 Battery SS Abt 500. LV Family: V-2. Launch Vehicle: V-2. FAILURE: Failure.
  • V-2 combat launch from Dalfsen - . Nation: Germany. Summary: Dalfsen, Estate Mataram, rocket fired, crashed in Wijhe near the farm De Hakke van J. Westhof in Marle..

1946 February 26 - .
  • XS-1 Flight 8 - . Crew: Woolams. Payload: XS-1 # 1 flight 8. Nation: USA. Related Persons: Woolams. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Bell flight 8. Dynamic stability check. At Pinecastle AAF, Florida..

1946 February 26 - .
  • XS-1 Flight 9 - . Crew: Woolams. Payload: XS-1 # 1 flight 9. Nation: USA. Related Persons: Woolams. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Bell flight 9. Rate of roll investigation. At Pinecastle AAF, Florida..

1947 February 26 - .
1953 February 26 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1021E.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1954 February 26 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1260T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1958 February 26 - .
  • Birth of Susan Jane Helms - . Nation: USA. Summary: American test engineer mission specialist astronaut. Flew on STS-54, STS-64, STS-78, STS-101, ISS EO-2. US Air Force flight test engineer..

1958 February 26 - . 02:35 GMT - . Launch Site: Kheysa. LV Family: V-2. Launch Vehicle: R-1. LV Configuration: A-1.
  • Ionosphere / aeronomy mission - . Nation: USSR. Agency: MVS. Apogee: 100 km (60 mi).

1958 February 26 - . 17:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC9. LV Family: Navaho. Launch Vehicle: Navaho G-26. LV Configuration: Navaho II SM-64 12. FAILURE: Booster shut down at T+20 seconds.. Failed Stage: 1.
  • Navaho G-26 Flight 9 - . Nation: USA. Agency: USAF. Apogee: 2.00 km (1.20 mi). Summary: The booster shut down at T+20 seconds in the flight. The vehicle was self-destructed by range safety before separation of the cruise stage had occurred..

1959 February 26 - . LV Family: Jupiter; Redstone.
  • Integration of the Mercury spacecraft with the Redstone and Jupiter launch vehicles. - . Nation: USA. Program: Mercury. Spacecraft: Mercury. Summary: Panel Number I (Design Subcommittee) met at Redstone Arsenal for the first time to discuss integration requirements for the Mercury spacecraft with the Redstone and Jupiter launch vehicles..

1960 February 26 - . 17:25 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas Agena A. LV Configuration: Atlas Agena A 29D / Agena A 1008. FAILURE: Second stage failed to separate.. Failed Stage: 2.
  • Midas 1 - . Payload: Midas / Agena TV 1008. Mass: 2,025 kg (4,464 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: Midas. Decay Date: 1960-02-26 . COSPAR: F600226A. Summary: Missile Defense Alarm System..

1962 February 26 - .
  • John Glenn Day in Washington, D.C. - . Nation: USA. Program: Mercury. Summary: This featured the reception of the astronaut at the White House, a parade, and his address to joint session of Congress..

1963 February 26 - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. FAILURE: Failure.
  • Mass spectrometer Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1964 February 26 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Lockheed recommendations on a scientific space station program. - . Nation: USA. Spacecraft: LORL. The Lockheed-California Company released details of its recommendations to MSC on a scientific space station program. The study concluded that a manned station with a crew of 24 could be orbiting the Earth in 1968. Total cost of the program including logistics spacecraft and ground support was estimated at $2.6 billion for five years' operation. Lockheed's study recommended the use of a Saturn V to launch the unmanned laboratory into orbit and then launching a manned logistics vehicle to rendezvous and dock at the station.

1964 February 26 - .
  • Soyuz plans - . Nation: USSR. Program: Lunar L1. Flight: Soyuz A-1; Soyuz A-2; Soyuz A-3; Soyuz A-4. Spacecraft: Soyuz A; Soyuz B; Soyuz V. The cosmonauts meet with engineers at TsNII-30 in Noginsk to review plans for docking trainers for the new Soyuz spacecraft. The trainers were supposed to be completed by now, but they are being held up for television and optical equipment to be delivered from Leningrad and Sverdlovsk. The mock-up of the 7K manned spacecraft trainer is immobile; it can only be turned around its centre of mass. The 1/30 scale of the 9K and 11K propulsion spacecraft with which the 7K will dock are free to rotate in all 3 axes. The cosmonauts in the 7K mock-up will see the 9K or 11K via the television screen aboard the spacecraft or in the Soyuz spacecraft in what the engineers promise will be a life-like appearance. They will practice approach and docking from a simulated distance of 300 m at a typical approach rate of 2 m/s. At the scale of the installation, this will equate to 10 cm/s. After the trainer review General Ioffe briefed the cosmonauts on plans for an electronic digital computer, with a mass of 40 kg, which was being developed for use in spacecraft navigation. Kamanin sees that very close collaboration will be needed between TsNII-30, TsPK, and GKNII VVS to complete trainer development on an accelerated schedule.

1964 February 26 - . Launch Site: Baikonur. LV Family: R-16. Launch Vehicle: R-16U. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1964 February 26 - . 01:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 437.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 26 - . 20:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-32.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 26 - . 21:18 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.124UA. FAILURE: Failure.
  • JHU Aurora 2 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 161 km (100 mi).

1965 February 26 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • A full-scale rehearsal of the flight crew countdown for Gemini-Titan 3 was conducted at the launch site. - . Nation: USA. Flight: Gemini 3. Procedures were carried out for moving the flight crew from their quarters in the Manned Spacecraft Center operations building at Merritt Island to the pilot's ready room at complex 16 at Cape Kennedy. Complete flight crew suiting operation in the ready room, the transfer to complex 19, and crew ingress into the spacecraft were practiced. Practice countdown proceeded smoothly and indicated that equipment and procedures were flight ready.

1965 February 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/3. LV Family: R-16. Launch Vehicle: R-16U.
  • PBG - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1965 February 26 - . 05:02 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92M. LV Configuration: Vostok 8A92M R15000-09.
  • Cosmos 58 - . Payload: Meteor no. 2. Mass: 4,730 kg (10,420 lb). Nation: USSR. Agency: Korolev. Class: Earth. Type: Weather satellite. Spacecraft: Meteor. Decay Date: 1990-02-25 . USAF Sat Cat: 1097 . COSPAR: 1965-014A. Apogee: 345 km (214 mi). Perigee: 333 km (206 mi). Inclination: 65.0000 deg. Period: 91.30 min. Summary: Probable weather satellite. Investigation of the upper atmosphere and outer space. .

1965 February 26 - . 11:10 GMT - . Launch Site: Eglin. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache Sphere 24.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 150 km (90 mi).

1965 February 26 - . 19:45 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-52-85.
  • X-15A MIT/AirD/Sky Bright Aeronomy mission - . Nation: USA. Agency: NASA; USAF. Apogee: 46 km (28 mi). Summary: Maximum Speed - 6034 kph. Maximum Altitude - 46817 m..

1966 February 26 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar PL87. LV Family: RT-2. Launch Vehicle: RT-2.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1966 February 26 - . 13:59 GMT - . Launch Site: Sonmiani. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.212IA.
  • Rehbar 10 (Na) Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1966 February 26 - . 16:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC34. LV Family: Saturn I. Launch Vehicle: Saturn IB. LV Configuration: Saturn IB SA-201.
  • Apollo 201 (AS-201) - . Nation: USA. Agency: NASA. Apogee: 488 km (303 mi). Apollo-Saturn 201 was launched from Cape Kennedy, with liftoff of an Apollo Block I spacecraft (CSM 009) on a Saturn IB launch vehicle at 11:12:01 EST. Launched from Launch Complex 34, the unmanned suborbital mission was the first flight test of the Saturn IB and an Apollo spacecraft. Total launch weight was 22,000 kilograms.

    Spacecraft communications blackout lasted 1 minute 22 seconds. Reentry was initiated with a space-fixed velocity of 29,000 kilometers per hour. CM structure and heatshields performed adequately. The CM was recovered by the USS Boxer from the Atlantic about 72 kilometers uprange from the planned landing point. (8.18 S x 11.15 W).


1968 February 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 116F.
  • ABRES BGRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi). Summary: The Boost Glide Re-entry Vehicle was launched from Vandenberg AFB, California to the area of Wake Island in the Pacific Ocean. It was launched from an Atlas missile booster and served to provide data on hypersonic manoeuvring flight characteristics..

1969 February 26 - . 07:47 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta E1. LV Configuration: Thor Delta E1 483/D67.
  • ESSA 9 - . Payload: TOS G. Mass: 145 kg (319 lb). Nation: USA. Agency: ESSA. Program: Tiros. Class: Earth. Type: Weather satellite. Spacecraft: TOS. USAF Sat Cat: 3764 . COSPAR: 1969-016A. Apogee: 1,505 km (935 mi). Perigee: 1,425 km (885 mi). Inclination: 101.8000 deg. Period: 115.20 min. Summary: Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..

1969 February 26 - . 08:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 267 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1969-03-06 . USAF Sat Cat: 3765 . COSPAR: 1969-017A. Apogee: 331 km (205 mi). Perigee: 202 km (125 mi). Inclination: 70.0000 deg. Period: 89.80 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1969 February 26 - . 10:00 GMT - . Launch Site: Thumba. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure ISRO-45.002.
  • ISRO 45.02 Ionosphere mission - . Nation: India. Agency: ISRO. Apogee: 145 km (90 mi).

1970 February 26 - .
  • Kamanin views DOS, continuation of N1-L3 with dismay - . Nation: USSR. Related Persons: Mishin. Program: Soyuz; Salyut; Lunar L3; Almaz. Flight: Soyuz 10; Soyuz 11. Spacecraft: Salyut 1; Soyuz 7K-LOK; LK; Almaz OPS; Soyuz OB-VI; Soyuz VI. The Ministry of Defence and VVS approve the draft DOS resolution. Kamanin has fought against it. He would prefer to develop a single reliable Soyuz spacecraft model by building and flying ten more (there are only four left of the original production lot in assembly). Instead the space leadership keep dreaming up new projects. In Kamanin's view, the DOS and its new Soyuz ferry design join Almaz, Soyuz VI, and the L3 as 'paper spacecraft'. Mishin still thinks he will 'teach the N1 to fly' and complete the L3, but Kamanin thinks the chances of this are nil. There is no coherent plan for Soviet spaceflight.

1970 February 26 - . 04:47 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark 2 S61/2.
  • ESRO S61 / 2 Aeronomy mission - . Nation: Europe. Agency: ESRO. Apogee: 225 km (139 mi).

1970 February 26 - . 13:30 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Apogee: 150 km (90 mi).

1970 February 26 - . 14:15 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Polar Atmospheric pressure Aeronomy/Ionosphere mission - . Nation: USSR. Apogee: 181 km (112 mi).

1971 February 26 - .
  • M2 Flight 22 - . Crew: Dana. Payload: M2-F3 flight 6. Nation: USA. Related Persons: Dana. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: M2-F3. Summary: Maximum Speed - 821 kph. Maximum Altitude - 13716 m. Flight Time - 348 sec..

1971 February 26 - . 05:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511L.
  • Cosmos 398 - . Payload: Lunar Craft T2K no. 2. Mass: 5,500 kg (12,100 lb). Nation: USSR. Agency: MOM. Program: Lunar L3. Class: Moon. Type: Manned lunar lander. Spacecraft: LK. Duration: 8,463.78 days. Decay Date: 1995-12-10 . USAF Sat Cat: 4966 . COSPAR: 1971-016A. Apogee: 1,958 km (1,216 mi). Perigee: 186 km (115 mi). Inclination: 51.5000 deg. Period: 106.70 min. Second space test of the LK moon lander test using the T2K version. Followed the same programme as Cosmos 379.
    Maneuver Summary:
    189km X 252km orbit to 186km X 1189km orbit. Delta V: 251 m/s
    186km X 1189km orbit to 200km X 10905km orbit. Delta V: 1320 m/s
    Total Delta V: 2832 m/s.
    Officially: Investigation of the upper atmosphere and outer space.

1971 February 26 - . 10:18 GMT - . Launch Site: Salto di Quirra. LV Family: Skylark. Launch Vehicle: Skylark 3 AC. LV Configuration: Skylark 3 AC S54. FAILURE: Failure.
  • ESRO S54 Solar x-ray mission - . Nation: Europe. Agency: ESRO. Apogee: 250 km (150 mi).

1972 February 26 - . 09:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1973 February 26 - . 03:23 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2. LV Configuration: Black Brant II ADD-2-127.
  • Auroral VUV Aurora / aeronomy / ionosphere mission - . Nation: Canada. Agency: NRCC. Apogee: 132 km (82 mi).

1974 February 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 February 26 - .
  • Kamanin in hospital. - . Nation: USSR. Summary: Kamanin has to go to the hospital for the first time in his life..

1975 February 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. LV Family: R-36M. Launch Vehicle: R-36M.
  • Missile accuracy test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 February 26 - . 09:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 710 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MK. Duration: 14.00 days. Decay Date: 1975-03-12 . USAF Sat Cat: 7675 . COSPAR: 1975-015A. Apogee: 335 km (208 mi). Perigee: 176 km (109 mi). Inclination: 65.0000 deg. Period: 89.60 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1975 February 26 - . 22:50 GMT - . Launch Site: Poker Flat. LV Family: Astrobee. Launch Vehicle: Astrobee D. LV Configuration: Astrobee D CRL A30.413-3.
  • Gerdian Condenser Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 104 km (64 mi).

1976 February 26 - . Launch Site: Natal. LV Family: Sonda. Launch Vehicle: Sonda 3. LV Configuration: Sonda 3 XV-01. FAILURE: Failure.
  • Serido test - . Nation: Brazil. Agency: IAE. Apogee: 47 km (29 mi).

1977 February 26 - .
  • Salyut 5 jettisons earth return capsule - . Nation: USSR. Spacecraft: KSI. Summary: The Earth Return Capsule serial number 11F76-0505 was successfully recovered. During the 1990's it was auctoned off at Sotheby's for $48,875..

1977 February 26 - . Launch Site: Eglin. Launch Complex: Eglin A-15. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac.
  • STRESS BETTY Aeronomy / ionosphere mission - . Nation: USA. Agency: DNA. Apogee: 500 km (310 mi).

1977 February 26 - . 20:02 GMT - . Launch Site: Fort Churchill. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.01UA.
  • Auroral NO Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 142 km (88 mi).

1977 February 26 - . 21:18 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Vostok 8A92M.
  • Cosmos 895 - . Payload: Tselina-D no. 11. Mass: 2,500 kg (5,500 lb). Nation: USSR. Agency: MOM. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. Decay Date: 1992-03-22 . USAF Sat Cat: 9853 . COSPAR: 1977-015A. Apogee: 442 km (274 mi). Perigee: 433 km (269 mi). Inclination: 81.2000 deg. Period: 93.30 min.

1978 February 26 - . 11:00 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-60.
  • Ultraviolet astronomy / extreme ultraviolet astronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 340 km (210 mi).

1979 February 26 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Final shuttle tests at NASA Huntsville - . Nation: USA. Summary: These verified loadings on the full mated shuttle stack with the external tank and solid rocket motors loaded with water to simulate the weights at various flight phases. 36 x 670 N and 20 x 4400 N exciters were used to vibrate the vehicle..

1979 February 26 - .
  • Complete mated vertical ground vibe test program - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Complete mated vertical ground vibration test program at MSFC, Enterprise (OV-101).

1979 February 26 - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.04UE.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1979 February 26 - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.03UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1979 February 26 - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Black Brant. Launch Vehicle: Black Brant 5A. LV Configuration: Black Brant VA AMF-VA-51.
  • Eclipse mission - . Nation: Canada. Agency: NRCC. Apogee: 132 km (82 mi).

1979 February 26 - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois GL A07.712-2.
  • Eclipse DEN Sphere Eclipse / aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 215 km (133 mi). Summary: Eclipse DEN. Launched from Red Lake, Chukuni Range, Ontario, Canada - Latitude: 50.88 N, Longitude:93.47 W..

1979 February 26 - . 16:28 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion GL A12.9A1.
  • Eclipse ASL-SE-79A1 Eclipse aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 158 km (98 mi). Summary: Eclipse ASL-SE-79A1. Launched from Red Lake, Chukuni Range, Ontario, Canada - Latitude: 50.88 N, Longitude:93.47 W..

1979 February 26 - . 16:28 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion GL A12.9B1.
  • Eclipse ASL-SE-79B1 Eclipse aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 158 km (98 mi). Summary: Eclipse ASL-SE-79B1. Launched from Red Lake, Chukuni Range, Ontario, Canada - Latitude: 50.88 N, Longitude:93.47 W..

1979 February 26 - . 16:51 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion GL A12.9A2.
  • Eclipse LWIR Eclipse / aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 141 km (87 mi). Summary: Eclipse LWIR. Launched from Red Lake, Chukuni Range, Ontario, Canada - Latitude: 50.88 N, Longitude:93.47 W..

1979 February 26 - . 16:52 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1021UE.
  • Eclipse Eclipse / aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 132 km (82 mi). Summary: Eclipse. Launched from Red Lake, Chukuni Range, Ontario, Canada - Latitude: 50.88 N, Longitude:93.47 W..

1979 February 26 - . 16:52 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Tomahawk Sandia. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk GL A10.802-1.
  • Eclipse / aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 115 km (71 mi).

1979 February 26 - . 16:54 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1022UE.
  • Eclipse Eclipse / aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 132 km (82 mi). Summary: Eclipse. Launched from Red Lake, Chukuni Range, Ontario, Canada - Latitude: 50.88 N, Longitude:93.47 W..

1979 February 26 - . 17:41 GMT - . Launch Site: Red Lake. Launch Complex: Red Lake CHK. LV Family: Tomahawk Sandia. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk GL A10.802-2.
  • Eclipse / aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 116 km (72 mi).

1980 February 26 - . 14:30 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1981 February 26 - . 20:30 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1982 February 26 - . 00:04 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 3910/PAM. LV Configuration: Delta 3910/PAM 644/D160.
  • Westar 4 - . Mass: 1,072 kg (2,363 lb). Nation: USA. Agency: WUTC. Program: Westar. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. Completed Operations Date: 1991-11-09 . USAF Sat Cat: 13069 . COSPAR: 1982-014A. Apogee: 35,943 km (22,333 mi). Perigee: 35,915 km (22,316 mi). Inclination: 2.0000 deg. Period: 1,443.40 min. TV, telephone. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit at 99 deg W in 1982-1991 As of 2 September 2001 located at 83.31 deg W drifting at 1.825 deg W per day. As of 2007 Mar 8 located at 112.98W drifting at 1.830W degrees per day.

1982 February 26 - . 03:50 GMT - . Launch Site: Fort Churchill. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.25UL.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 160 km (90 mi).

1982 February 26 - . 20:10 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-53 - . Payload: Molniya-1T. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1T. USAF Sat Cat: 13070 . COSPAR: 1982-015A. Apogee: 38,895 km (24,168 mi). Perigee: 1,456 km (904 mi). Inclination: 63.2000 deg. Period: 717.70 min. Replaced Molniya 1-47. Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network.

1983 February 26 - . 18:50 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1986 February 26 - . 12:02 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. Launch Pad: LC35?. LV Family: Black Brant. Launch Vehicle: Black Brant 5B. LV Configuration: Black Brant VB NASA 21.93UG.
  • JHU FOT 6 Halley Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 229 km (142 mi).

1986 February 26 - . 13:40 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1734 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 59.00 days. Decay Date: 1986-04-26 . USAF Sat Cat: 16618 . COSPAR: 1986-020A. Apogee: 343 km (213 mi). Perigee: 165 km (102 mi). Inclination: 67.1000 deg. Period: 89.60 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1987 February 26 - . Launch Site: Sonde Stromfjord. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX GL A21.628.
  • POLAR ARC / COPE II Plasma mission - . Nation: USA. Agency: USAF. Apogee: 387 km (240 mi).

1987 February 26 - . 13:30 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1824 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 55.00 days. Decay Date: 1987-04-22 . USAF Sat Cat: 17559 . COSPAR: 1987-021A. Apogee: 352 km (218 mi). Perigee: 162 km (100 mi). Inclination: 67.2000 deg. Period: 89.70 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1987 February 26 - . 23:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 3914. LV Configuration: Delta 3914 D179.
  • GOES 7 - . Payload: GOES H. Mass: 399 kg (879 lb). Nation: USA. Agency: NOAA. Class: Earth. Type: Weather satellite. Spacecraft: GOES. Completed Operations Date: 1998-01-01 . USAF Sat Cat: 17561 . COSPAR: 1987-022A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 1.2000 deg. Period: 1,436.20 min. Stationed at 83 deg W. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit at 75 deg W in 1987-1988; 108 deg W in-98 deg W in 1989-1992; 111 deg W in 1992; 112 deg W in 1993-1994; 135 deg W in 1995; 98 deg W in 1996-1998 As of 5 September 2001 located at 179.83 deg E drifting at 0.023 deg W per day. As of 2007 Mar 9 located at 176.12W drifting at 0.061W degrees per day.

1987 February 26 - . 23:43 GMT - . Launch Site: Sonde Stromfjord. LV Family: Terrier. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.25UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).

1988 February 26 - . 09:00 GMT - .
1988 February 26 - . 09:31 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 1922 - . Payload: Oko #56. Mass: 1,800 kg (3,900 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. USAF Sat Cat: 18881 . COSPAR: 1988-013A. Apogee: 34,181 km (21,239 mi). Perigee: 6,225 km (3,868 mi). Inclination: 67.6000 deg. Period: 718.80 min. Summary: Covered Oko constellation plane 5 - 75 degree longitude of ascending node..

1989 February 26 - . 11:46 GMT - . Launch Site: Ascension. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 65 km (40 mi).

1990 February 26 - . 02:06 GMT - . Launch Site: Andoya. LV Family: S. Launch Vehicle: S-520. LV Configuration: S-520-12.
  • Auroral mission - . Nation: Japan. Agency: ISAS. Apogee: 369 km (229 mi).

1991 February 26 - . 04:53 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/3. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47168-254.
  • Cosmos 2135 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 21130 . COSPAR: 1991-013A. Apogee: 1,018 km (632 mi). Perigee: 923 km (573 mi). Inclination: 82.8000 deg. Period: 104.50 min. Summary: Military navigation satellite. Replaced by Cosmos 2195. Reactivated in August 1993 after Cosmos 2195 failed..

1992 February 26 - . 23:58 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V49.
  • Superbird B1 - . Mass: 2,560 kg (5,640 lb). Nation: Japan. Agency: SCC. Program: Superbird. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 21893 . COSPAR: 1992-010A. Apogee: 36,206 km (22,497 mi). Perigee: 36,057 km (22,404 mi). Inclination: 0.9000 deg. Period: 1,453.80 min. Stationed at 162 deg E. Domestic communications. Launching organization Arianespace. Launch time 2358 GMT. Positioned in geosynchronous orbit at 162 deg E in 1992-1999 As of 4 September 2001 located at 19.90 deg W drifting at 4.382 deg W per day. As of 2007 Mar 9 located at 164.51E drifting at 4.378W degrees per day.
  • Arabsat 1C - . Mass: 1,310 kg (2,880 lb). Nation: Arab States. Agency: Arabsat. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 100. USAF Sat Cat: 21894 . COSPAR: 1992-010B. Apogee: 35,808 km (22,250 mi). Perigee: 35,763 km (22,222 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Stationed at 31 deg E. Positioned in geosynchronous orbit at 31 deg E in 1992-1997; 55 deg E in 1998-1999 As of 5 September 2001 located at 55.07 deg E drifting at 0.005 deg E per day. As of 2007 Mar 9 located at 172.70E drifting at 5.710W degrees per day.

1993 February 26 - . 20:45 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands LC42. LV Family: Polaris. Launch Vehicle: STARS. LV Configuration: STARS FTU-1.
  • FTU-1 test - . Nation: USA. Agency: USA SDC. Apogee: 900 km (550 mi).

1997 February 26 - . 20:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.161NP.
  • DARTFire 3 Microgravity mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1998 February 26 - . 07:07 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F20.
  • SNOE - . Nation: USA. Agency: NASA Greenbelt. Manufacturer: Colorado. Program: STEDI. Class: Earth. Type: Seismology satellite. Spacecraft: SNOE. Decay Date: 2003-12-13 . USAF Sat Cat: 25233 . COSPAR: 1998-012A. Apogee: 581 km (361 mi). Perigee: 529 km (328 mi). Inclination: 97.7000 deg. Period: 95.80 min. Summary: SNOE, the Student Nitric Oxide Explorer. Small satellite built by the University of Colorado to measure the Nitric Oxide density as a function of altitude. First satellite in the STEDI (Student Explorer Demonstration Initiative) program..
  • Teledesic 1 - . Payload: BATSAT. Nation: USA. Agency: Teledesic. Manufacturer: Germantown. Class: Communications. Type: Civilian communications satellite. Spacecraft: Teledesic. Decay Date: 2000-10-09 . USAF Sat Cat: 25234 . COSPAR: 1998-012B. Apogee: 577 km (358 mi). Perigee: 532 km (330 mi). Inclination: 97.7000 deg. Period: 95.70 min. Summary: Communications Technology Demonstrator..

1999 February 26 - . 22:44 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V116.
  • Arabsat 3A - . Mass: 2,708 kg (5,970 lb). Nation: Arab States. Agency: Arabsat. Manufacturer: Cannes. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 25638 . COSPAR: 1999-009A. Apogee: 35,792 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. The Arab League satellite had 20 Ku-band transponders and was to be stationed at 26 degrees East. Dry mass was 1200 kg. Positioned in geosynchronous orbit at 26 deg E in 1999. As of 29 August 2001 located at 25.93 deg E drifting at 0.007 deg E per day. As of 2007 Mar 9 located at 25.89E drifting at 0.003E degrees per day.
  • Skynet 4E - . Mass: 1,490 kg (3,280 lb). Nation: UK. Agency: MoD. Manufacturer: Stevenage. Program: Skynet. Class: Communications. Type: Military communications satellite. Spacecraft: ECS/OTS. USAF Sat Cat: 25639 . COSPAR: 1999-009B. Apogee: 35,796 km (22,242 mi). Perigee: 35,777 km (22,230 mi). Inclination: 7.2000 deg. Period: 1,436.10 min. Skynet 4E was a SHF/UHF military communications satellite for the UK Ministry of Defense. Dry mass was 759 kg; it used a Thiokol Star 30 solid apogee motor. Stationed at 53 deg E. Positioned in geosynchronous orbit at 53 deg E in 1999. As of 5 September 2001 located at 52.91 deg E drifting at 0.000 deg W per day. As of 2007 Mar 11 located at 53.02E drifting at 0.005E degrees per day.

2000 February 26 - .
  • Death of Petr Aleksandrovich Tyurin - . Nation: Russia. Related Persons: Tyurin, Petr. Summary: Russian chief designer. Chief Designer 1953-1981 of KB Arsenal. Specialised in L3 components and later performed EORSAT work..

2000 February 26 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 730. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-51.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

2000 February 26 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 730. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-51.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

2000 February 26 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 730. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-51.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

2000 February 26 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 730. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-51.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

2000 February 26 - . 09:19 GMT - . Launch Site: Poker Flat. Launch Complex: Poker Flat LC4. LV Family: Black Brant. Launch Vehicle: Black Brant 12. LV Configuration: Black Brant XII NASA 40.15IE.
  • GEODESIC Ionosphere mission - . Nation: Canada. Agency: CSA. Apogee: 990 km (610 mi).

2001 February 26 - . 08:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U 670 / ISS-3P.
  • Progress M-44 - . Payload: Progress M s/n 244. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-1. Spacecraft: Progress M. Duration: 49.22 days. Decay Date: 2001-04-16 . USAF Sat Cat: 26713 . COSPAR: 2001-008A. Apogee: 393 km (244 mi). Perigee: 376 km (233 mi). Inclination: 51.6000 deg. Period: 92.20 min. ISS Servicing flight. Launch delayed from February10/20. Progress M-44 was a Russian, automatic cargo carrier that carried 2.5 tonnes of food, water, fuel, oxygen, and equipment to the International Space Station. In preparation for the docking, the ISS crew repositioned the Soyuz TM-31 escape craft from its port on Zvezda to a port on the Zarya module. Progress M-44 docked with the -Y port on Zvezda at 09:47 UT on 28 February. It undocked from Zvezda's aft port on April 16 at 0848 GMT and was deorbited at 1323 GMT over the Pacific Ocean.

2004 February 26 - .
  • International Space Station Status Report #04-11 - . Nation: USA. Related Persons: Foale; Kaleri. Program: ISS. Flight: ISS EO-8. The residents of the International Space Station today conducted the first ever two-man spacewalk without a crewmember inside, but the planned five and a half hour-spacewalk to support technology experiments and prepare for a future visit from a cargo vehicle was cut short by a cooling system problem with one of the two crewmembers' Russian Orlan suits. Additional Details: International Space Station Status Report #04-11.

2005 February 26 - . 09:25 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 2022. LV Configuration: H-IIA 2022 H-IIA-7F.
  • Himawari 6 - . Payload: MT-Sat 1R. Mass: 3,300 kg (7,200 lb). Nation: Japan. Agency: MLIT. Manufacturer: Palo Alto. Class: Earth. Type: Weather satellite. Spacecraft: FS-1300. USAF Sat Cat: 28622 . COSPAR: 2005-006A. Apogee: 35,798 km (22,243 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. Return to flight after earlier failure; first commercial mission for H-2A. Delayed from August 2003, January 2004, and February 24, 2005. The dual-purpose satellite was to provide weather data for the Japanese Meteorological Agency (as with others in the Himawari-GMS series), and air traffic control support (airplane-ATC voice/data links, GPS augmentation and airplane position tracking) for the Japanese Civil Aviation Bureau. As of 2007 Mar 11 located at 140.26E drifting at 0.000E degrees per day.

2008 February 26 - .
  • ISS On-Orbit Status 02/26/08 - . Nation: USA. Related Persons: Eyharts; Love; Malenchenko; Whitson. Program: ISS. Flight: ISS EO-16; STS-123. Concluding his first session with the NASA/JSC experiment NUTRITION w/Repository, FE-2 Eyharts completed the all-day Part 2, by collecting urine samples for 24 hrs, to continue through tomorrow morning.

    The samples were consecutively stored in the MELFI (Minus-Eighty Laboratory Freezer for ISS). Blood collections were performed by Peggy on Leo yesterday. (The current NUTRITION/Repository project is the most comprehensive in-flight study done by NASA to date of human physiologic changes during long-duration space flight. It includes measures of bone metabolism, oxidative damage, nutritional assessments, and hormonal changes, expanding the previous Clinical Nutritional Assessment profile (MR016L) testing in three ways: Addition of in-flight blood & urine collection (made possible by MELFI), normative markers of nutritional assessment, and a return session plus 30-day (R+30) session to allow evaluation of post-flight nutrition and implications for rehabilitation.) Additional Details: ISS On-Orbit Status 02/26/08.


2009 February 26 - . 18:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-3SLB. LV Configuration: Zenit-3SLB s/n LL2.
  • Telstar 11N - . Mass: 4,012 kg (8,844 lb). Nation: Canada. Agency: SIS. Program: Telstar. Spacecraft: FS-1300. USAF Sat Cat: 34111 . COSPAR: 2009-009A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ku-band direct-broadcast satellite with 39 high-power transponders covering North and Central America, Europe, Africa and the Atlantic Ocean Region, stationed at 37.5 degrees..

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. Nation: Russia. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 37372 . COSPAR: 2011-009A. Apogee: 19,147 km (11,897 mi). Perigee: 19,111 km (11,875 mi). Inclination: 64.8000 deg. Period: 675.70 min. Summary: Navigation satellite..

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