Encyclopedia Astronautica
January 11


January 11 Chronology


1610 January 11 - .
  • Galileo Galilei's Discovery of Jupiter Moon Ganymede - . Nation: Italy.

1787 January 11 - .
  • William Herschel's Discovery of Uranus Moons Titania and Oberon - . Nation: UK.

1908 January 11 - .
1920 January 11 - .
  • Smithsonian publishes Goddard's "A Method of Reaching Extreme Altitudes" - . Nation: USA. Related Persons: Goddard. Summary: Goddard's work lays out the concept of using the multi-stage rocket for exploration of outer space and reaching the lunar surface. It spawns a nightmare of media interest and derision, making Goddard even more secretive of his dreams for space flight..

1926 January 11 - .
1944 January 11 - . Launch Site: Peenemuende. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-082.
1945 January 11 - . Launch Site: Peenemuende. Launch Complex: Peenemuende SK. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 20821.
  • V-2 Ma379 V3 - . Nation: Germany. Summary: Planned range 320 km. Launched into sea; accuracy 14.7 km to the right of the planned trajectory. Circular error 38.0 km from aim point. 'Kitz' launch - listed under Heidekraut launches, but actually made from Karlshagen or railhead area of Peenemuende..

1946 January 11 - . LV Family: Atlas. Launch Vehicle: Atlas.
  • Strategic Missile Proposals - . Nation: USA. Bids were received in response to the USAAF request for proposal of the previous October. Vultee submitted proposals for two types (glide and ballistic) of 8000-km range missiles. North American proposed a three-year development program for a supersonic 800-km range missile, culminating in a production run of 50 missiles.

1946 January 11 - . LV Family: Hermes. Launch Vehicle: Hermes.
  • Hermes Mach 3 ramjet proposed. - . Nation: USA. Related Persons: von Braun. Summary: Von Braun briefs Hermes; V-2 first stage, ramjet second stage, cruise at 3400 kph at 19 km altitude..

1949 January 11 - . Launch Site: Wallops Island.
  • First canted rocket nozzle test. - . Nation: USA. Summary: First launching of a rocket model employing known but nonaerodynamic torque from canted rocket nozzles, for determining damping in roll of wings, at NACA's Wallops Island, Va..

1949 January 11 - . Launch Site: Wallops Island. LV Family: HVAR. Launch Vehicle: HVAR.
  • D13 model test flight - . Nation: USA. Agency: NASA. Apogee: 5.00 km (3.10 mi).

1950 January 11 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Deacon.
  • F26 Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1954 January 11 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1200A.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1955 January 11 - . LV Family: Navaho. Launch Vehicle: Navaho G-26.
  • Navaho G-26 second production contract - . Nation: USA. Program: Navaho. Summary: This added 12 more cruise stages, 21 boosters, and 6 N6 navigation systems, bringing the total procured to 22 cruise stages, 34 boosters, and 11 navigation systems..

1957 January 11 - . LV Family: R-7. Launch Vehicle: R-7A.
  • First Soviet ICBM base at Plesetsk is authorised. - . Nation: USSR. Summary: Decree 61-39ss 'On creation of launch complex Angara at NIIP-53' was issued..

1957 January 11 - . LV Family: R-7. Launch Vehicle: R-7.
  • Flight test program for R-7 approved. - . Nation: USSR. Summary: Decree 'On approval of flight-testing program for the R-7 ICBM' was issued..

1958 January 11 - . Launch Site: Point Mugu. LV Family: Polaris. Launch Vehicle: Polaris TV.
  • FBM Test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1960 January 11 - .
  • Contract signed by NASA and the Western Electrice for the Mercury tracking network. - . Nation: USA. Program: Mercury. Summary: A contract (NAS 1-430) was signed by NASA and the Western Electric Company in the amount of $33,058,690 for construction and engineering of the Mercury tracking network..

1960 January 11 - .
  • Star City cosmonaut training centre approved. - . Nation: USSR. Summary: Soviet Air Froce Decree 'On creation of the Cosmonaut Training Centre' was issued..

1961 January 11 - .
  • Progress made in mapping the moon - . Nation: USA. Program: Apollo. John Blake of the Air Force Aeronautical Chart and Information Center (ACIC) described to STG representatives the progress made by ACIC in mapping the moon. Lunar maps to the scale of 1: 5,000,000 and 1: 10,000,000 were later requested and received by STG. In addition, the first two sheets of a projected 144 sheet map coverage of the lunar surface on a 1:1,000,000 scale were forwarded to STG by the Center.

1961 January 11 - . 18:40 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 601. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1E-15. FAILURE: Failure.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 20 km (12 mi).

1962 January 11 - .
  • In State of the Union message Kennedy discusses moon program - . Nation: USA. Related Persons: Kennedy. Program: Apollo. In his State of the Union message to the Congress, President John F . Kennedy said: "With the approval of this Congress, we have undertaken in the past year a great new effort in outer space. Our aim is not simply to be first on the moon, any more than Charles Lindbergh's real aim was to be first to Paris. His aim was to develop the techniques and the authority of this country and other countries in the field of the air and the atmosphere, and our objective in making this effort, which we hope will place one of our citizens on the moon, is to develop in a new frontier of science, commerce and cooperation, the position of the United States and the free world. This nation belongs among the first to explore it. And among the first - if not the first - we shall be."

1962 January 11 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: Kosmos 3. Launch Vehicle: R-14U.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 675 km (419 mi).

1963 January 11 - .
  • Korolev lays out detailed plan for future Vostok flights - . Nation: USSR. Flight: Vostok 5; Vostok 6; Vostok 6A; Vostok 7; Vostok 8; Vostok 9; Vostok 10. Korolev and Kamanin meet to lay out Vostok flight plan. There were three variants possible for the March flights: 1) A single female flight of 2 to 3 days; 2) Two female flights launched one day apart, but landing at the same time; 3) An 'absurd' version: launch of a female cosmonaut for a three day flight, followed two days after her landing by a male cosmonaut on a 5 to 7 day flight. The planners selected the two female flight variant.

1964 January 11 - .
  • Three U S Air Force test pilots in a simulated seven- day lunar landing mission - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Simulator. Three U. S. Air Force test pilots began a five-week training period at the Martin Company leading to their participation in a simulated seven- day lunar landing mission. This was part of Martin's year-long study of crew performance during simulated Apollo missions (under a $771,000 contract from NASA).

1964 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2. LV Configuration: Thor SLV-2A Agena D 390 / Agena D 2354.
  • Agena D 2354 - . Mass: 700 kg (1,540 lb). Nation: USA. Agency: USAF. Program: ELINT. Spacecraft: Ferret. USAF Sat Cat: 727 . COSPAR: 1964-001A. Apogee: 937 km (582 mi). Perigee: 906 km (562 mi). Inclination: 69.9000 deg. Period: 103.50 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • Solrad 7A; NRL Solar Rad - . Payload: GRAB 5. Mass: 45 kg (99 lb). Nation: USA. Agency: NRL. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: GRAB. USAF Sat Cat: 730 . COSPAR: 1964-001D. Apogee: 920 km (570 mi). Perigee: 902 km (560 mi). Inclination: 69.9000 deg. Period: 103.20 min. Summary: Solar radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • Unidentified - . Payload: NRL PL135. Mass: 40 kg (88 lb). Nation: USA. Agency: NRL. Program: ELINT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: NRL ELINT. USAF Sat Cat: 731 . COSPAR: 1964-001E. Apogee: 919 km (571 mi). Perigee: 902 km (560 mi). Inclination: 69.9000 deg. Period: 103.20 min. Summary: Identified by McDowell as probable NRL ELINT satellite..
  • GGSE 1 - . Mass: 39 kg (85 lb). Nation: USA. Agency: NRL. Class: Technology. Type: Gravity gradient technology satellite. Spacecraft: GGSE. USAF Sat Cat: 728 . COSPAR: 1964-001B. Apogee: 916 km (569 mi). Perigee: 899 km (558 mi). Inclination: 69.9000 deg. Period: 103.20 min. Summary: Gravity gradient stabilization tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • SECOR 1 - . Payload: EGRS 1. Mass: 18 kg (39 lb). Nation: USA. Agency: USA. Class: Earth. Type: Geodetic satellite. Spacecraft: SECOR. USAF Sat Cat: 729 . COSPAR: 1964-001C. Apogee: 922 km (572 mi). Perigee: 904 km (561 mi). Inclination: 69.9000 deg. Period: 103.30 min. Summary: Located Pacific islands. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1965 January 11 - .
  • LC 16 to be converted to test stands for Apollo - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Structural. NASA announced that Kennedy Space Center's Launch Complex 16, a Titan missile facility, would be converted into static test stands for Apollo spacecraft. This decision eliminated the need for such a facility originally planned on Merritt Island and, it was predicted, would cost little more than a fourth of the $7 million estimated for the new site.

1965 January 11 - .
  • Dalmo-Victor to supply antennas for Apollo CSM's - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Communications. North American selected Dalmo-Victor to supply S-band high-gain antennas for Apollo CSM's. (The deployable antenna would be used beyond 14,816 km (8,000 nm) from the earth.) Dalmo-Victor would complete the antenna design and carry out the development work, and North American would procure production units under a supplemental contract.

1965 January 11 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 632. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-67.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1965 January 11 - . 09:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92. LV Configuration: Vostok 8A92 R15002-03.
  • Cosmos 52 - . Payload: Zenit-2 11F61 s/n 26. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: Korolev. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 8.00 days. Decay Date: 1965-01-19 . USAF Sat Cat: 968 . COSPAR: 1965-001A. Apogee: 298 km (185 mi). Perigee: 203 km (126 mi). Inclination: 65.0000 deg. Period: 89.50 min. Summary: Area survey photo reconnaissance satellite..

1966 January 11 - .
  • Female flight go-ahead - . Nation: USSR. Related Persons: Tyulin; Ponomaryova; Solovyova; Yerkina; Kuznetsova. Program: Voskhod. Flight: Voskhod 5. Spacecraft: Voskhod; Berkut. Summary: Tyulin has ordered the crew for the female Voskhod flight to enter final flight training and the preparation of all necessary space suits, cabin uniforms, crew couch liners, documentation, and other final preparations..

1967 January 11 - . Launch Site: Vandenberg.
  • First and only launch of a Castor/Scramjet - . Nation: USA. Summary: First and only launch of a Castor/Scramjet from Vandenberg AFB..

1967 January 11 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique 61. LV Configuration: Veronique 61 VA84.
  • FU-161 Astronomy X-ray astronomy / ultraviolet astronomy mission - . Nation: France. Agency: CNES. Apogee: 158 km (98 mi). Summary: FU161 X-ray and UV astronomy / Stab mission..

1967 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 4300C. Launch Pad: 4300C. LV Family: Sergeant. Launch Vehicle: Castor.
  • Marquardt Scramjet Technology mission - . Nation: USA. Agency: USAF AFSC. Apogee: 54 km (33 mi).

1967 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2073.
  • Force modification research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 January 11 - . 10:55 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta E1. LV Configuration: Thor Delta E1 468/D44.
  • Intelsat 2 F-2 - . Mass: 87 kg (191 lb). Nation: International. Agency: INTELSAT. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 2. Completed Operations Date: 1977-05-01 . USAF Sat Cat: 2639 . COSPAR: 1967-001A. Apogee: 35,808 km (22,250 mi). Perigee: 35,769 km (22,225 mi). Inclination: 1.6000 deg. Period: 1,436.20 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Pacific Ocean at 174 deg E in 1967-1969; over the Pacific Ocean 162-170 deg E in 1969-1970; over the Pacific Ocean 150-160 deg E in 1970-1975 As of 7 August 2001 located at 48.66 deg E drifting at 0.413 deg W per day. As of 2007 Mar 8 located at 63.48W drifting at 0.357W degrees per day.

1968 January 11 - .
  • Apollo Parachute Test Vehicle failed - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Parachute. A Parachute Test Vehicle (PTV) test failed at El Centro, Calif. The PTV was released from a B-52 aircraft at 15,240 meters and the drogue chute programmer was actuated by a static line connected to the aircraft. One drogue chute appeared to fail upon deployment, followed by failure of the second drogue seven seconds later. Additional Details: Apollo Parachute Test Vehicle failed.

1968 January 11 - . Launch Site: Green River. Launch Complex: Green River Pad 2. LV Family: Athena RTV. Launch Vehicle: Athena RTV. LV Configuration: Athena B022.
  • USAF B022 re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1968 January 11 - . 16:16 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Delta E1. LV Configuration: Thor Delta E1 454/D56.
  • Explorer 36 - . Payload: GEOS B. Mass: 209 kg (460 lb). Nation: USA. Agency: NASA Greenbelt. Program: Explorer. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: GEOS. USAF Sat Cat: 3093 . COSPAR: 1968-002A. Apogee: 1,574 km (978 mi). Perigee: 1,081 km (671 mi). Inclination: 105.8000 deg. Period: 112.20 min. The geodetic instrumentation systems included (1) four optical beacons, (2) two C-band radar transponders, (3) a passive radar reflector, (4) a sequential collation of range radio range transponder, (5) a Goddard range and range rate transponder, (6) laser reflectors, and (7) Doppler beacons. Non-geodetic systems included a laser detector and a Minitrack interferometer beacon. The objectives of the spacecraft were to optimise optical station visibility periods and to provide complementary data for inclination-dependent terms established by the Explorer 29 (GEOS 1) gravimetric studies. The spacecraft was placed into a retrograde orbit to accomplish these objectives. Operational problems occurred in the main power system, optical beacon flash system, and the spacecraft clock, and adjustments in scheduling resulted in nominal operations.

1969 January 11 - . LV Family: N1. Launch Vehicle: N1.
  • N1 state commission meeting. - . Nation: USSR. Related Persons: Afanasyev, Sergei. Program: Lunar L3; Lunar L1. Spacecraft: Soyuz 7K-L1A. Summary: The issues raised with the N1 have been cleared up and settled. Afanasyev approves the schedule leading to an 18 February first launch of the N1..

1970 January 11 - .
  • Funeral arrangements for Belyayev - . Nation: USSR. Related Persons: Belyayev. Kamanin is making state funeral arrangements for Belyayev. The question is -- shall he be given the same send-off as Gagarin and Komarov, or less? Word comes down from the Kremlin - less. He is to be buried not in the Kremlin wall at Red Square, but in Novodevich Cemetary.

1971 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-30 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 January 11 - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800024.
  • SAFEGUARD M1-30 Interceptor mission - . Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1971 January 11 - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800021.
  • SAFEGUARD M1-30 Interceptor mission - . Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1972 January 11 - .
  • SL-1 should be flown at an altitude of 435 km - . Nation: USA. Program: Skylab. MSC proposed that SL-1 should be flown at an altitude of 435 km and that the orbit should be controlled by removing any insertion dispersions and drag effects with burns of the SL 2 CSM reaction control system after that spacecraft had rendezvoused and docked with SL-1. Additional Details: SL-1 should be flown at an altitude of 435 km.

1973 January 11 - . 10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 543 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4M. Duration: 13.00 days. Decay Date: 1973-01-24 . USAF Sat Cat: 6339 . COSPAR: 1973-002A. Apogee: 274 km (170 mi). Perigee: 191 km (118 mi). Inclination: 64.9000 deg. Period: 89.20 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1974 January 11 - . Launch Site: White Sands. LV Family: Arcas. Launch Vehicle: Arcas.
  • Gerdien condenser Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 70 km (43 mi).

1975 January 11 - . 00:32 GMT - . Launch Site: Cape Parry. LV Family: Black Brant. Launch Vehicle: Black Brant 4B. LV Configuration: Black Brant IVB Tordo II.
  • Periquito Plasma / barium release mission - . Nation: Canada. Agency: Sandia. Apogee: 540 km (330 mi).

1975 January 11 - . 10:53 GMT - . Launch Site: Sonde Stromfjord. LV Family: Black Brant. Launch Vehicle: Black Brant 4B.
  • DLR G-BB4-66 Ionosphere mission - . Nation: USA. Agency: DFVLR. Apogee: 280 km (170 mi).

1976 January 11 - . 17:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 92 km (57 mi).

1977 January 11 - . 21:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1978 January 11 - . 23:55 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • STERETOP Active Plasma mission - . Nation: USSR. Agency: AN. Apogee: 150 km (90 mi).

1979 January 11 - . 15:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1070 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 9.00 days. Decay Date: 1979-01-20 . USAF Sat Cat: 11229 . COSPAR: 1979-001A. Apogee: 293 km (182 mi). Perigee: 205 km (127 mi). Inclination: 62.8000 deg. Period: 89.50 min. Summary: Area survey photo reconnaissance satellite; returned film capsule..
  • Nauka Cosmos 1070 - . Payload: Nauka. Nation: USSR. Agency: MOM. Spacecraft: Nauka. Decay Date: 1979-01-27 . USAF Sat Cat: 11245 . COSPAR: 1979-001F. Apogee: 280 km (170 mi). Perigee: 199 km (123 mi). Inclination: 62.8000 deg. Period: 89.29 min.

1980 January 11 - . 12:28 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-46 - . 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. Decay Date: 1992-10-22 . USAF Sat Cat: 11662 . COSPAR: 1980-002A. Apogee: 28,891 km (17,952 mi). Perigee: 103 km (64 mi). Inclination: 63.2000 deg. Period: 500.30 min. Summary: Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network..

1981 January 11 - . 20:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1982 January 11 - . 19:24 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 72 km (44 mi).

1983 January 11 - . 20:15 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1984 January 11 - . 12:20 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1530 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1984-01-25 . USAF Sat Cat: 14622 . COSPAR: 1984-002A. Apogee: 362 km (224 mi). Perigee: 189 km (117 mi). Inclination: 72.9000 deg. Period: 90.00 min. Summary: Photo surveillance; returned film capsule..

1984 January 11 - . 18:08 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65039-546.
  • Cosmos 1531 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 14624 . COSPAR: 1984-003A. Apogee: 1,006 km (625 mi). Perigee: 980 km (600 mi). Inclination: 82.9000 deg. Period: 105.00 min. Summary: Military navigation satellite. Replaced Cosmos 1386..

1987 January 11 - . 20:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1988 January 11 - . 19:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1989 January 11 - . 15:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1990 January 11 - . 18:01 GMT - .
  • EVA Mir EO-5-2 - . Crew: Viktorenko; Serebrov. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.12 days. Nation: USSR. Related Persons: Viktorenko; Serebrov. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-5. Spacecraft: Mir. Summary: Retrieved and installed material samples.

1992 January 11 - . 03:40 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 36.079UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 248 km (154 mi).

1994 January 11 - .
  • Mir News 203: Soyuz-TM18 docked with the Mir-space station. - . Nation: Russia. Program: Mir. Flight: Mir EO-15; Mir EO-14; Mir LD-4. On 10.01.94 at 1050 UTC Soyuz-TM18 docked to the Mir-station. Approach and docking took place in the automatic mode by the use of the system Kurs. During Mir's pass in orbit 45144 (1138-1147 UTC) the approach was going on. Afanasyev watched the behaviour of Soyuz-TM18 on his monitor. He had to be alert to take over manually, but this was not necessary. Soyuz-TM18 approached and docked smoothly. During the approach the transmitter of Mir and of the Soyuz-TM18 as well could be heard. During the pass in the next orbit (45145, 1315-1323 UTC) the hatch was opened and the enthusiastic welcome and greetings of both crews could be monitored. The following pass (orb. 45146, 1448-1459 UTC) Serebrov spoke a word of welcome and reported that mood and health of the newcomers were excellent. For Dr. Polyakov reason to gather blood samples from the cosmonauts to be able to confirm this scientifically.

    The 5 men will work together during the next 3 days and the old crew (Mir Main expedition nr. 14) will then hand over the station to the 15th Main expedition.

    On 14.01.1994 Tsibliyev and Serebrov will return to earth in the Soyuz-TM17.

    The 15th Main Expedition will last until 6.07.1994, so 177 days. Then Afanasyev and Usachev will be relieved by Malenchenko, Musabayev and Strekalov. Strekalov will return with the relieved crew. Dr. Polyakov will remain on board until spring 1995 (427 days) to conduct medical experiments aimed at the long-lasting flights to Mars.

    Chris v.d. Berg, NL-9165/A-UK3202


1995 January 11 - .
  • Mir News 241: Autonomous test flight Soyuz-TM20 - . Nation: Russia. Program: Mir. Flight: Mir EO-17; Mir LD-4. On 11.01.1995 between 0900 and 0925 UTC the Soyuz-TM20 flew autonomously to test the Kurs-approach and docking system at the forward transition section (P.Kh.O.) of the Mir-complex. Problems during some docking operations in Aug/Sept 1994 (Progress-M24) and on 6.10.1994 (Soyuz-TM20) made this operation necessary. Long before Soyuz-TM20 separated from the complex the whole crew was on board of that ship and thoroughly tested all systems. According to the plan the Soyuz-TM20 executed the approach and docking fully automatically by use of the Kurs system. Viktorenko, assisted by Kondakova, was ready to take over manually if something went wrong or in case of a too high fuel consumption. Soyuz-TM20 perfectly linked to the station at 09.24.57 UTC, the aberrations remained far within the limits, just before docking less than 0.5 degrees. The good functioning of the Kurs systems is indispensable for the execution of the program for this year. During the operation with the Soyuz-TM20 the radio traffic went via the geostationary Altair. During the separation Soyuz-TM20 flew within our range and the traffic could be monitored on 121.750 mc as well as via Altair.

    Luch-1:

    This geostationary satellite to be used for Mir-TsUP communications in the near future is standing over 95 degrees East, but is not yet operational for TDRS purposes.

    Chris van den Berg, NL-9165/A-UK3202


1996 January 11 - . 09:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39B. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-72.
  • STS-72 - . Call Sign: Endeavour. Crew: Barry; Chiao; Duffy; Jett; Scott, Winston; Wakata. Payload: Endeavour F10 / OAST / FSU. Mass: 6,510 kg (14,350 lb). Nation: USA. Related Persons: Barry; Chiao; Duffy; Jett; Scott, Winston; Wakata. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-72. Spacecraft: Endeavour. Duration: 8.92 days. Decay Date: 1996-01-20 . USAF Sat Cat: 23762 . COSPAR: 1996-001A. Apogee: 310 km (190 mi). Perigee: 302 km (187 mi). Inclination: 28.5000 deg. Period: 90.60 min. Summary: Deployed and retrieved OAST Flyer; retrieved SFU Space Flyer Unit. Beside the two satellite retrievals, the mission included two spacewalks..
  • SLA-1/GAS - . Nation: USA. Agency: NASA. Program: STS. Decay Date: 1996-01-20 . USAF Sat Cat: 23762 . COSPAR: 1996-001xx. Apogee: 310 km (190 mi). Perigee: 302 km (187 mi). Inclination: 28.5000 deg. Period: 90.60 min.
  • OAST-Flyer - . Nation: USA. Agency: NASA Greenbelt. Class: Technology. Type: Navigation technology satellite. Spacecraft: OAST-Flyer. Decay Date: 1996-01-20 . USAF Sat Cat: 23763 . COSPAR: 1996-001B. Apogee: 311 km (193 mi). Perigee: 301 km (187 mi). Inclination: 28.5000 deg. Period: 90.60 min. Summary: GPS receiver, amateur radio tests; examined effect of solar radiation on satellite explosive devices; deployed from STS 72 1/14/96; retrieved 1/16/96..

2001 January 11 - .
  • The release of the Congressionally-chartered Space Commission report set the stage for significant organizational and mission changes for Air Force Space Command. - . Nation: USA.

2002 January 11 - .
  • ISS Status Report: ISS 02-02 - . Nation: USA. Related Persons: Bursch; Onufrienko; Walz. Program: ISS. Flight: ISS EO-4. The Expedition Four crew is completing its fifth week in space aboard the International Space Station, continuing preparations for the first spacewalk of the five-month mission. The six-hour spacewalk by Commander Yury Onufrienko and Flight Engineer Carl Walz is scheduled to begin at 2:56 p.m. CST, Monday, Jan. 14. This week, with the assistance of their crewmate, Flight Engineer Dan Bursch, the two spacewalkers outfitted and tested their Russian Orlan spacesuits and prepared the tools and equipment they will use on Monday. Additional Details: ISS Status Report: ISS 02-02.

2004 January 11 - . 04:13 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL 12.
  • Estrela do Sul 1 (Skynet Brazil 1, Telstar 14) - . Mass: 4,694 kg (10,348 lb). Nation: Brazil. Agency: Skynet. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28137 . COSPAR: 2004-001A. Apogee: 35,794 km (22,241 mi). Range: 0 km ( mi). Perigee: 35,779 km (22,231 mi). Period: 1,436.10 min. Initially planned for launch on Delta 4M+ (4,2). Launch delayed from January 10. Placed in geosynchronous orbit but reports indicated there were problems deploying one of the solar panels. As of 2007 Mar 11 located at 63.07W drifting at 0.006W degrees per day.

2007 January 11 - . 22:28 GMT - . Launch Site: Xichang. LV Family: DF-21. Launch Vehicle: DF-21. LV Configuration: DF-21 ASAT 3.
  • Chinese ASAT destroys FY-1C target satellite. - . Nation: China. Agency: PRC. Apogee: 850 km (520 mi). The FY-1C satellite, launched on 10 May 1999, was presumably well past the end of its operational life. It was destroyed in a test of a Chinese ASAT weapon at an altitude of 850 km, 4 degrees west of Xichang. Launch vehicle was unknown, but a version of the DF-21 IRBM would be sufficient to reach that altitude. Reportedly the flight had been preceded by one to three earlier tests that were either failures or just aimed at a point in space. The program was apparently very secret, and the Chinese foreign ministry was caught by surprise by the test and the storm of international condemnation that followed. The FY-1C was blown into over 200 pieces of debris, adding immediately by 10% to the population of space junk that threatens lower-altitude satellites.

2008 January 11 - .
  • ISS On-Orbit Status 01/11/08 - . Nation: USA. Related Persons: Love; Malenchenko; Tani; Whitson; Williams, Dave. Program: ISS. Flight: ISS EO-16; ISS EO-16-1; STS-122. CDR Whitson and FE-2 Tani started out with the daily reading of SLEEP (Sleep-Wake Actigraphy and Light Exposure during Spaceflight) experiment data accumulated during the night, for logging and filling in questionnaire entries in the SLEEP session file on the HRF-1 laptop for downlink.

    (To monitor the crewmembers' sleep/wake patterns and light exposure, Dan and Peggy wear a special Actiwatch device which measures the light levels encountered by him as well as his patterns of sleep and activity throughout the Expedition. The log entries are done within 15 minutes of final awakening for seven consecutive days, as part of the crew's discretionary 'job jar' task list.)

    At ~3:10am EST, the FE-2 activated the VDS MPC (Video Distribution System/Multi-Purpose Converter) with its four downlinks to allow the ground to conduct HDTV (high-definition TV) playback and downlink operations. Later (~11:30am), the MPC was powered off again. Additional Details: ISS On-Orbit Status 01/11/08.


2010 January 11 - . 11:55 GMT - . Launch Site: Jiuquan.
  • Target - . Nation: China. Apogee: 100 km (60 mi). Summary: Target.

2010 January 11 - . 12:00 GMT - . Launch Site: Urumqi. LV Family: DF-21. Launch Vehicle: DF-21.
  • Interceptor - . Nation: China. Apogee: 100 km (60 mi). Summary: ABM test.

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