Encyclopedia Astronautica
January 25


January 25 Chronology


1907 January 25 - .
  • Birth of Norair Martirosovich Sisakyan - . Nation: Russia. Summary: Russian scientist. Early space medicine specialist at the Second Division of Biological Sciences under the Academy of Sciences..

1943 January 25 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-011.
  • V-2 4011 - . Nation: Germany. Agency: Wehrmacht. Summary: Steep roll; Burnout at T+64.5 seconds. Range 105 km.

1944 January 25 - . Launch Site: Peenemuende. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-074.
1945 January 25 - . Launch Site: Peenemuende. Launch Complex: Peenemuende SK. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 20829. FAILURE: Failed 1300 m above pad.
  • V-2 Ma385 V8 - . Nation: Germany. Summary: Planned range 320 km. 'Kitz' launch - listed under Heidekraut launches, but actually made from Karlshagen or railhead area of Peenemuende..

1950 January 25 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Deacon.
  • X-3 Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1951 January 25 - . 15:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-10. LV Configuration: Aerobee RTV-N-10 A20.
  • Ozone Aeronomy mission - . Nation: USA. Agency: APL. Apogee: 90 km (55 mi). Summary: Solar radiation research. Launched at 0800 local time. Reached 90.1 km..

1952 January 25 - . Launch Site: Holloman. Launch Complex: Holloman SLED. LV Family: Snark. Launch Vehicle: MX-775.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1952 January 25 - . Launch Site: Le Cardonnet. LV Family: Veronique. Launch Vehicle: Veronique P6. LV Configuration: Veronique P6 P6-1.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 1.00 km (0.60 mi).

1954 January 25 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1280T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1955 January 25 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1E. LV Configuration: R-1E 1.
  • Test / biology mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi). Summary: Payload section deployed at 22 seconds. Left animal container recovered. Carried dogs..

1956 January 25 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-54-18.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1958 January 25 - .
  • Dynasoar request for proposal - . Nation: USA. Spacecraft: Dynasoar. After surveying 111 potential bidders, the USAF issued Requests for Proposal to ten companies (Bell, Boeing, Vought, Convair, Douglas, General Electric, Lockheed, Martin, North American, Western Electric). Later McDonnell, Northrop, and Republic were also issued RFP's.

1958 January 25 - . 19:12 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun AM6.02.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 157 km (97 mi).

1959 January 25 - .
  • Mercury pilot egress trainer received. - . Nation: USA. Program: Mercury. Spacecraft: Mercury. Summary: The pilot egress trainer was received from McDonnell and rough water evaluation of the equipment was started immediately by Space Task Group personnel..

1960 January 25 - .
  • McDonnell delivered first production Mercury spacecraft. - . Nation: USA. Program: Mercury. Spacecraft: Mercury. McDonnell delivered the first production-type Mercury spacecraft to the Space Task Group at Langley in less than 1 year from the signing of the formal contract. This spacecraft was a structural shell and did not contain most of the internal systems that would be required for manned space flight. After receipt, the Space Task Group instrumented the spacecraft and designated it for the Mercury-Atlas 1 (MA-1) flight.

1961 January 25 - .
  • Study on the feasibility of refueling a spacecraft in orbit - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Source Selection; LM Mode Debate; LM Source Selection. Summary: NASA announced that the Lockheed Aircraft Corporation had been awarded a contract by the Marshall Space Flight Center to study the feasibility of refueling a spacecraft in orbit..

1962 January 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. LV Family: R-16. Launch Vehicle: R-16U.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1962 January 25 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 408.
  • Research and development launch - . Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi).

1962 January 25 - . 22:02 GMT - . Launch Site: Point Mugu. LV Family: Nike Zeus. Launch Vehicle: Nike Zeus.
  • PM-7 Sim target - . Nation: USA. Agency: USA. Apogee: 150 km (90 mi).

1963 January 25 - . 10:44 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 39D. FAILURE: Failure. Failed Stage: 1.
  • NTMP K-9/OT ABM test - . Nation: USA. Agency: USAF SAC. Apogee: 100 km (60 mi).

1964 January 25 - .
  • Soviet Air Force Cosmonaut Training Group 2 Supplemental selected. - . Nation: USSR. Related Persons: Beregovoi. The group was selected to provide experienced test pilot for the Soyuz manned spaceflight program.. Qualifications: Personal selection.. Beregovoi was a very experienced test pilot, but older than the official age criteria. However he had the support of leading figures in the space program. He joined the cosmonaut team on a 'special basis' in 1964.

1964 January 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: Tsiklon. Launch Vehicle: R-36 8K67. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1964 January 25 - . 05:30 GMT - . Launch Site: Thumba. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.79UE UNH64-1.
  • ISRO 20.01? E'jet Magnetospheric mission - . Nation: USA. Agency: NASA. Apogee: 164 km (101 mi).

1964 January 25 - . 13:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor Agena B SLV-2. LV Configuration: Thor SLV-2 Agena B 397 (TA2) / Agena B 6301.
  • Echo 2 - . Payload: Echo C A-12. Mass: 256 kg (564 lb). Nation: USA. Agency: NASA Langley. Class: Technology. Type: Communications technology satellite. Spacecraft: Echo 2. Decay Date: 1969-06-07 . USAF Sat Cat: 740 . COSPAR: 1964-004A. Apogee: 1,315 km (817 mi). Perigee: 1,030 km (640 mi). Inclination: 81.5000 deg. Period: 108.80 min. Summary: Passive commsat; balloon; 1st joint US/USSR space mission. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .

1965 January 25 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • Gemini launch vehicle 3 was erected at complex 19. - . Nation: USA. Flight: Gemini 3. Summary: Power was applied January 29 and Subsystems Functional Verification Tests (SSFVT) commenced. SSFVT were finished February 12. The Combined Systems Test before spacecraft mating was conducted February 15-16..

1965 January 25 - .
  • Backup Apollo Block II space suit development program - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; A7L; CSM Block II. MSC negotiated a backup Block II space suit development program with David Clark Company, which paralleled the Hamilton Standard program, at a cost of $176,000. Criteria for selecting the suit for ultimate development for Block II would be taken from the Extravehicular Mobility Unit Design and Performance Specification. A selection test program would be conducted at MSC using the CM mockup, the lunar simulation facility, and the LEM mockup.

1965 January 25 - .
  • Optimism permeated Apollo program - . Nation: USA. Related Persons: Seamans. Program: Apollo. The optimism that permeated the Apollo program was reflected in statements by NASA's Associate Administrator, Robert C. Seamans, Jr., during budget briefings for the forthcoming year. He was "greatly encouraged" by recent design freezes and "very reassured" by testing of propulsion systems and launch vehicle stages. "We really feel," Seamans said, ". . . that we can get off the (lunar landing) flight on an earlier mission than I would have said a year ago?' Certainly it was "conceivable" that the moon landing could come "in early 1970."

1965 January 25 - . 16:00 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2B. LV Configuration: Black Brant IIB CC-2B-48.
  • Test mission - . Nation: Canada. Agency: NRCC. Apogee: 230 km (140 mi).

1965 January 25 - . 20:53 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2B. LV Configuration: Black Brant IIB CC-2B-56. FAILURE: Failure.
  • Test mission - . Nation: Canada. Agency: NRCC. Apogee: 20 km (12 mi).

1966 January 25 - . Launch Site: White Sands. Launch Complex: White Sands LC50. Launch Vehicle: Sprint. LV Configuration: Sprint ABM FLA-2. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 0 km ( mi).

1966 January 25 - . 01:52 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.158UA.
  • Spheres Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 167 km (103 mi).

1966 January 25 - . 12:28 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC86/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 106 - . Payload: DS-P1-I s/n 1. Mass: 325 kg (716 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-I. Completed Operations Date: 1966-11-15 . Decay Date: 1966-11-14 . USAF Sat Cat: 1949 . COSPAR: 1966-004A. Apogee: 553 km (343 mi). Perigee: 281 km (174 mi). Inclination: 48.4000 deg. Period: 92.80 min. Summary: Operational radar target for the ABM forces..

1967 January 25 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100. FAILURE: Failure.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1967 January 25 - . 03:00 GMT - . Launch Site: Cape Canaveral. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk MUMP-7 (ETR-0851).
  • Aeronomy / ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 327 km (203 mi).

1967 January 25 - . 13:55 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC162/36. LV Family: Tsiklon. Launch Vehicle: R-36-O. LV Configuration: R-36O 8K69 N22500 No. 07L.
  • Cosmos 139 - . Mass: 1,700 kg (3,700 lb). Nation: USSR. Agency: RVSN. Class: Military. Type: Orbital bombing system. Spacecraft: OGCh. Decay Date: 1967-01-25 . USAF Sat Cat: 2656 . COSPAR: 1967-005A. Apogee: 210 km (130 mi). Perigee: 144 km (89 mi). Inclination: 49.7000 deg. Period: 88.00 min. Summary: Third orbital Fractional Orbital Bombardment System test. First apparently successful test. The warhead was braked to an impact in the Kapustin Yar range..

1967 January 25 - . 23:16 GMT - . Launch Site: Dumont d'Urville. LV Family: Belier. Launch Vehicle: Dragon 1. LV Configuration: Dragon D-24.
  • FU-145B ionosphere / particles Ionosphere mission - . Nation: France. Agency: CNES. Apogee: 340 km (210 mi).

1968 January 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF22. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2448.
  • ST Olympic Trials 7 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 January 25 - . LV Family: N1. Launch Vehicle: N1.
  • Apollo vs Ye-8-5 - . Nation: USSR. Program: Lunar L3; Luna; Apollo. Flight: Apollo 9. Spacecraft: Luna Ye-8-5. America is preparing Apollo 9 for flight, and Kamanin muses that the Soviet reply will be the N1 and Ye-8-5, neither of which is proven or reliable. The Soviet Union would have a better chance of sending a manned L1 on a flight around the moon during the first quarter of 1969. Meanwhile Mishin's bureau has a new L3M lunar lander on the drawing boards. This will land 4 to 5 men on the moon, but require two N1 or seven UR-500K launches to assemble in orbit.

1969 January 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2A. FAILURE: Payload propulsion system failed; no orbit.. Failed Stage: P.
  • US-A Mass Model - . Mass: 3,800 kg (8,300 lb). Nation: USSR. Agency: RVSN. Program: RORSAT. Class: Surveillance. Type: Military naval surveillance radar satellite. Spacecraft: US-A. Decay Date: 1969-01-24 . COSPAR: F690125A. Apogee: 100 km (60 mi). Summary: RORSAT hardware, representative of production hardware, but using chemical batteries in place of BES-5 nuclear reactor..

1969 January 25 - . 03:00 GMT - . Launch Site: White Sands. LV Family: Loki. Launch Vehicle: Super Loki.
  • Meteorological Sphere Aeronomy mission - . Nation: USA. Agency: USA. Apogee: 126 km (78 mi).

1969 January 25 - . 21:00 GMT - . Launch Site: Kiruna. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.316IM.
  • RTG SNC 2A / 4 Aeronomy mission - . Nation: Sweden. Agency: NASA; RTG. Apogee: 118 km (73 mi).

1970 January 25 - . 02:20 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.270UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 169 km (105 mi).

1970 January 25 - . 05:00 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-28.
  • Ionosphere mission - . Nation: Japan. Agency: ISAS. Apogee: 369 km (229 mi).

1971 January 25 - .
  • Cosmonauts on public relations duty. - . Nation: USSR. Summary: A record number of cosmonauts are away from the training centre on public relations trips..

1971 January 25 - . 08:19 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.324GE.
  • PCA particle spectra Plasma mission - . Nation: USA. Agency: NASA. Apogee: 160 km (90 mi).

1971 January 25 - . 11:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.318UA.
  • JHU UVT F6 (Venus) Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 160 km (90 mi).

1971 January 25 - . 12:38 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C60/1.
  • ESRO C60 / 1 Chemical release / particles mission - . Nation: Europe. Agency: ESRO. Apogee: 175 km (108 mi).

1971 January 25 - . 14:26 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.46UA.
  • JHU Airglow 10 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 245 km (152 mi).

1971 January 25 - . 15:12 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.432GE.
  • PCA particle spectra Plasma mission - . Nation: USA. Agency: NASA. Apogee: 160 km (90 mi).

1972 January 25 - . 11:15 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 472 - . Payload: DS-P1-Yu s/n 52. Mass: 250 kg (550 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-Yu. Completed Operations Date: 1972-08-16 . Decay Date: 1972-08-18 . USAF Sat Cat: 5804 . COSPAR: 1972-004A. Apogee: 1,536 km (954 mi). Perigee: 193 km (119 mi). Inclination: 82.0000 deg. Period: 102.20 min. Summary: Development of systems for air defence and the control of outer space..

1973 January 25 - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800039.
  • Safeguard M2-26 Interceptor mission - . Nation: USA. Agency: USA. Apogee: 150 km (90 mi).

1973 January 25 - . 01:15 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: Cockatoo.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 122 km (75 mi).

1974 January 25 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100N.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 January 25 - . 11:30 GMT - . Launch Site: El Arenosillo. LV Family: Skua. Launch Vehicle: Skua 4. LV Configuration: Skua 4 MS4CLO-7403.
  • Ionosphere mission - . Nation: UK. Agency: INTA; DLR. Apogee: 109 km (67 mi).

1975 January 25 - . 12:40 GMT - . Launch Site: El Arenosillo. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel M P GFD-75001.
  • Ionosphere mission - . Nation: UK. Agency: INTA. Apogee: 100 km (60 mi).

1976 January 25 - . 23:20 GMT - . Launch Site: Syowa Base. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210JA-22.
  • NO / Ne Aeronomy / ionosphere mission - . Nation: Japan. Agency: NIPR. Apogee: 127 km (78 mi).

1977 January 25 - .
  • Complete aft fuselage assembly on dock, STA-099 - . Nation: USA. Program: STS. Summary: Complete aft fuselage assembly on dock, Palmdale (STA-099).

1977 January 25 - . 01:30 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima T. LV Family: S. Launch Vehicle: TT-500. LV Configuration: TT-500 TT-500-1F.
  • Test mission - . Nation: Japan. Agency: NASDA. Apogee: 300 km (180 mi).

1978 January 25 - . 14:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 78 km (48 mi).

1979 January 25 - . 05:43 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92M.
  • Meteor 1-29 - . Payload: Meteor-Priroda s/n 2-3. Mass: 3,800 kg (8,300 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Weather satellite. Spacecraft: Meteor-Priroda. USAF Sat Cat: 11251 . COSPAR: 1979-005A. Apogee: 596 km (370 mi). Perigee: 546 km (339 mi). Inclination: 97.8000 deg. Period: 96.10 min. Obtaining information needed for research into the natural resources of the earth and the development of methods for remote sensing of the underlying surface, and obtaining meteorological information. In addition to Soviet apparatus, carried scientific ap paratus from the German Democratic Republic.

1979 January 25 - . 21:07 GMT - . Launch Site: Kiruna. LV Family: Petrel. Launch Vehicle: Petrel 2. LV Configuration: Petrel 2 P216K.
  • Auroral pulsations Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 179 km (111 mi).

1980 January 25 - . 20:36 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47164-249.
  • Cosmos 1153 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 11680 . COSPAR: 1980-007A. Apogee: 1,014 km (630 mi). Perigee: 961 km (597 mi). Inclination: 82.9000 deg. Period: 104.90 min. Summary: Military navigation satellite..

1981 January 25 - . 20:40 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1982 January 25 - . 16:00 GMT - . Launch Site: Natal. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki FLIGHT 297 /TN1-.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 67 km (41 mi).

1983 January 25 - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47193-480. FAILURE: Launch vehicle failed to orbit - unknown cause.. Failed Stage: U.
  • Romb - . Nation: USSR. Agency: UNKS. Class: Military. Type: Radar calibration target. Spacecraft: Taifun-2. COSPAR: F830125J. Summary: Carried Romb radar calibration subsatellites..

1984 January 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT100GM Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1984 January 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT99GM Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1984 January 25 - . 16:09 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 36 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 112 km (69 mi).

1984 January 25 - . 16:39 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-124.
  • Ferdinand 67 M-T 4 Aeronomy mission - . Nation: Norway. Agency: NTNF; DLR. Apogee: 118 km (73 mi).

1984 January 25 - . 18:13 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 37 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 115 km (71 mi).

1986 January 25 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
  • Meteorological Chaff Meteorological mission - . Nation: India. Agency: ISRO. Apogee: 70 km (43 mi).

1987 January 25 - . 20:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1988 January 25 - . 02:00 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-81.
  • COREX Ionosphere mission - . Nation: Japan. Agency: ISAS. Apogee: 359 km (223 mi).

1989 January 25 - .
1989 January 25 - .
  • IMBP Cosmonaut Training Group 5 selected. - . Nation: USSR. Related Persons: Karashtin; Lukyanyuk; Morukov. Summary: Physicians and biomedical specialist cosmonauts for planned missions to the Mir space station..

1989 January 25 - .
  • Buran Cosmonaut Training Group 3 selected. - . Nation: USSR. Related Persons: Polonski. Summary: Experienced test pilots were selected to train for manned missions using the Buran space shuttle..

1989 January 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT131GB Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1990 January 25 - . 17:15 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2057 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 53.00 days. Decay Date: 1990-03-19 . USAF Sat Cat: 20457 . COSPAR: 1990-009A. Apogee: 330 km (200 mi). Perigee: 183 km (113 mi). Inclination: 62.8000 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..

1991 January 25 - . 19:23 GMT - . Launch Site: Scud Batteries. Launch Pad: IRAQ-S. LV Family: R-17. Launch Vehicle: Al Hussein.
  • Riyadh - . Nation: Iraq. Apogee: 100 km (60 mi).

1991 January 25 - . 19:23 GMT - . Launch Site: Scud Batteries. Launch Pad: IRAQ-S. LV Family: R-17. Launch Vehicle: Al Hussein.
  • Riyadh - . Nation: Iraq. Apogee: 100 km (60 mi).

1992 January 25 - . 07:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 R15000-058.
  • Progress M-11 - . Payload: Progress M s/n 212. Mass: 7,320 kg (16,130 lb). Nation: Russia. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-10; Mir LD-3. Spacecraft: Progress M. Duration: 48.33 days. Completed Operations Date: 1992-03-13 13:13:31 . Decay Date: 1992-03-13 13:13:31 . USAF Sat Cat: 21851 . COSPAR: 1992-004A. Apogee: 227 km (141 mi). Perigee: 185 km (114 mi). Inclination: 51.6000 deg. Period: 88.60 min. Summary: Unmanned resupply vessel to Mir. Docked with Mir on 27 Jan 1992 09:30:43 GMT. Undocked on 13 Mar 1992 08:43:40 GMT. Destroyed in reentry on 13 Mar 1992 15:47:00 GMT. Total free-flight time 2.36 days. Total docked time 45.97 days..

1994 January 25 - . 00:25 GMT - . Launch Site: Plesetsk. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Meteor 3-06 - . Payload: Meteor-3 s/n 7. Mass: 2,150 kg (4,730 lb). Nation: Russia. Agency: RAKA. Class: Earth. Type: Weather satellite. Spacecraft: Meteor-3. USAF Sat Cat: 22969 . COSPAR: 1994-003A. Apogee: 1,228 km (763 mi). Perigee: 1,191 km (740 mi). Inclination: 82.0000 deg. Period: 109.40 min. Obtained meterological and solar-terrestrial data. Meteor 3-6 was inserted into an orbital plane 60 degrees to the west of Meteor 3-5's plane and ejected the small German satellite Tubsat B on the second orbit. Meteor 3-6 also carried an integrated French radiometer called SCARAB (Scanner for Radiation Budget) and a German PRARE (Precision Range and Range Rate Experiment) geodetic instrument. The French radiometer was designed to study the Earth's radiation budget over an extended period of time and to measure the effect of clouds on the greenhouse phenomenon. A second SCARAB instrument was manifested on a Meteor spacecraft that was to be launched in 1996, but this did not come to pass. The German PRARE was similar to the instrument carried on ESA's ERS· 1 satellite.
  • Tubsat-B - . Mass: 40 kg (88 lb). Nation: Germany. Agency: TUB. Program: Tubsat. Class: Technology. Type: Navigation technology satellite. Spacecraft: Tubsat. USAF Sat Cat: 22970 . COSPAR: 1994-003B. Apogee: 1,210 km (750 mi). Perigee: 1,184 km (735 mi). Inclination: 82.6000 deg. Period: 109.40 min. Following the success of the magnetic torque attitude control system that flew on Tubsat-A, researchers and students at Germany's Technical University of Berlin constructed Tubsat-B to test and demonstrate attitude control with a star sensor and three reaction wheels. An on-board 1m telescope was used for astronomy and for Earth observation at 10m resolution. Dimensions of the satellite were 38x38x50 cm, mass 40 kg. Unfortunately communications with the satellite were lost after 39 Days

1994 January 25 - . 16:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 2G. LV Configuration: Titan II SLV 23G-11 / M68B-67 + M68B-89.
  • Clementine 1 - . Payload: Clementine 1 / DSPSE-ISA [Star-37FM]. Mass: 424 kg (934 lb). Nation: USA. Agency: BMDO. Class: Moon. Type: Lunar probe. Spacecraft: Clementine. USAF Sat Cat: 22973 . COSPAR: 1994-004A. Apogee: 409,890 km (254,690 mi). Perigee: 804 km (499 mi). Inclination: 63.8000 deg. Period: 16,158.80 min. SDIO sensor technology demonstration; mapped lunar surface; planned asteroid flyby cancelled due to spacecraft failure. After two Earth flybys, lunar insertion was achieved on February 21. Lunar mapping took place over approximately two months, in two parts. The first part consisted of a 5 hour elliptical polar orbit with a perilune of about 400 km at 28 degrees S latitude. After one month of mapping the orbit was rotated to a perilune of 29 degrees N latitude, where it remained for one more month. This allowed global imaging as well as altimetry coverage from 60 degrees S to 60 degrees N. After leaving lunar orbit, a malfunction in one of the on-board computers on May 7 at 14:39 UTC (9:39 AM EST) caused a thruster to fire until it had used up all of its fuel, leaving the spacecraft spinning at about 80 RPM with no spin control. This made the planned continuation of the mission, a flyby of the near-Earth asteroid Geographos, impossible. The spacecraft remained in geocentric orbit and continued testing the spacecraft components until the end of mission. Additional Details: Clementine 1.
  • ISA - . Payload: ISA. Nation: USA. Agency: BMDO. Class: Technology. Type: Military technology satellite. Decay Date: 1994-06-08 . USAF Sat Cat: 22987 . COSPAR: 1994-004C. Apogee: 126,958 km (78,887 mi). Perigee: 396 km (246 mi). Inclination: 65.8000 deg. Period: 3,075.57 min.

1995 January 25 - . 06:24 GMT - . Launch Site: Andoya. Launch Complex: Andoya U3. LV Family: Black Brant. Launch Vehicle: Black Brant 12. LV Configuration: Black Brant XII NASA 40.06IE.
  • SCIFER Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 1,453 km (902 mi).

1995 January 25 - . 22:40 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-2E. LV Configuration: Chang Zheng 2E CZ2E-5 (37). FAILURE: Shortcomings in the guidance system lead to the vehicle not anticipating the true effects of horizontal wind-shear once the mountains surrounding the launch site were cleared. This caused the nose fairing to collapse and the spacecraft to be destroyed.. Failed Stage: G.
  • Apstar 2 - . Nation: China. Agency: PRC. Program: Apstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 601. Decay Date: 1995-01-25 . COSPAR: F950125A. Because the Apstar failure happened a few seconds later than Optus, the consequences were catastrophic. The vehicle was destroyed, and the falling wreckage landed on a village down-range of the launch site, killing at least 20 and perhaps as many as 120 people.

1996 January 25 - . 09:56 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 374-02.
  • Gorizont 31 - . Payload: Gorizont s/n 43L. Mass: 2,125 kg (4,684 lb). Nation: Russia. Agency: MOM. Class: Communications. Type: Civilian communications satellite. Spacecraft: Gorizont . USAF Sat Cat: 23775 . COSPAR: 1996-005A. Apogee: 35,801 km (22,245 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.9000 deg. Period: 1,436.20 min. Summary: Stationed at 39.8E. Positioned in geosynchronous orbit at 40 deg E in 1996-1999 As of 5 September 2001 located at 40.11 deg E drifting at 0.042 deg W per day. As of 2007 Mar 11 located at 74.36E drifting at 1.416W degrees per day..

1998 January 25 - . 08:35 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K. LV Family: S. Launch Vehicle: S-310. LV Configuration: S-310-27.
  • SEEK Ozone Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 183 km (113 mi).

2000 January 25 - . 01:04 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 42L. LV Configuration: Ariane 42L-3 V126.
  • Galaxy 10R - . Payload: Galaxy XR. Mass: 1,987 kg (4,380 lb). Nation: USA. Agency: PanAmSat. Manufacturer: El Segundo. Program: Galaxy. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 601. USAF Sat Cat: 26056 . COSPAR: 2000-002A. Apogee: 35,978 km (22,355 mi). Perigee: 35,950 km (22,330 mi). Inclination: 3.2000 deg. Period: 1,445.20 min. Geosynchronous communications satellite launched to supplement Panamsat's Galaxy cable TV distribution constellation. It carried Ku and C band transponders and was to be stationed at 127 deg W. A replacement for Galaxy 10, lost on the first Delta 3 launch failure. Stationed at 123 deg W. Positioned in geosynchronous orbit at 123 deg W in 2000. As of 3 September 2001 located at 122.99 deg W drifting at 0.002 deg E per day. As of 2007 Mar 11 located at 123.03W drifting at 0.000E degrees per day.

2000 January 25 - . 16:45 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-4 (60).
  • Zhongxing-22 - . Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Manufacturer: CAST. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: FH-1. USAF Sat Cat: 26058 . COSPAR: 2000-003A. Apogee: 35,794 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 3.2000 deg. Period: 1,436.10 min. First Chinese military communications satellite. Perhaps an update of the DFH-3 design. Stationed at 98 deg E. The first in a planned constellation of satellites to be launched through 2010. Positioned in geosynchronous orbit at 98 deg E in 2000. As of 5 September 2001 located at 98.03 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 97.95E drifting at 0.009W degrees per day.

2001 January 25 - .
  • ISS Status Report: ISS 01-04 - . Nation: USA. Related Persons: Gidzenko; Shepherd. Program: ISS. Flight: ISS EO-1. Nearing the end of their third month in space, the three-member Expedition 1 crew spent a smooth but busy week aboard the International Space Station, practicing emergency procedures, performing routine maintenance and inspections, and preparing for the continued expansion of the station with the launch of the Space Shuttle Atlantis next month. Additional Details: ISS Status Report: ISS 01-04.

2002 January 25 - . 03:15 GMT - . Launch Site: Balasore. LV Family: Agni. Launch Vehicle: Agni 1.
  • Agni RV Mk 2 - . Nation: India. Agency: IDRDL. Apogee: 300 km (180 mi).

2002 January 25 - . 15:19 GMT - .
  • EVA ISS EO-4-2 - . Crew: Bursch; Onufrienko. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.26 days. Nation: USA. Related Persons: Bursch; Onufrienko. Program: ISS. Flight: ISS EO-4. The astronauts installed plume deflectors around the Zvezda thrusters and set up some exposure experiments. The Pirs airlock was depressurized probably about 1510 UTC, with hatch open at 1519 UTC; hatch close was at 2118 UTC and repressurization began at 2120 UTC.

2003 January 25 - . 20:13 GMT - . Launch Site: Mayport DZ. Launch Pad: 29.0 N x 78.5 W. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F32.
  • SORCE - . Payload: Solstice/SAVE. Mass: 268 kg (590 lb). Nation: USA. Agency: NASA. Manufacturer: OSC. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: SORCE. USAF Sat Cat: 27651 . COSPAR: 2003-004A. Apogee: 657 km (408 mi). Perigee: 617 km (384 mi). Inclination: 39.9946 deg. Period: 97.31 min. Summary: Solar irradiance monitoring, climatology mission. Launch delayed from December 1 and 13, 2002..

2004 January 25 - .
  • Opportunity Rover Mars Landing - . Nation: USA. Spacecraft: MER.

2004 January 25 - .
  • Mars Exploration Rover B (Opportunity), Mars Landing, Successful - . Nation: USA. Spacecraft: MER.

2005 January 25 - . 01:30 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A.
  • ROMA 2005 RWFS19 Aeronomy mission - . Nation: USA. Agency: DLR. Apogee: 90 km (55 mi).

2008 January 25 - .
  • ISS On-Orbit Status 01/25/08 - . Nation: USA. Related Persons: Eyharts; Malenchenko; Tani; Whitson. Program: ISS. Flight: ISS EO-16. 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.)

    Upon wakeup, FE-1 Yuri Malenchenko terminated his eighth MBI-12 SONOKARD experiment session, started last night, by taking the recording device from his SONOKARD sports shirt pocket and later copying the measurements to the RSE-MED laptop for subsequent downlink to the ground. (SONOKARD objectives are stated to (1) study the feasibility of obtaining the maximum of data through computer processing of records obtained overnight, (2) systematically record the crewmember's physiological functions during sleep, (3) study the feasibility of obtaining real-time crew health data. Investigators believe that contactless acquisition of cardiorespiratory data over the night period could serve as a basis for developing efficient criteria for evaluating and predicting adaptive capability of human body in long-duration space flight.) Additional Details: ISS On-Orbit Status 01/25/08.


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