Encyclopedia Astronautica
June 26


June 26 Chronology


1925 June 26 - .
1939 June 26 - .
  • Birth of Ansar Ilgamovich Sharafutdinov - . Nation: Russia. Summary: Tatar-Russian pilot cosmonaut, 1965-1968. Cosmonaut training November 1965 - December 1967. Withdrawn from cosmonaut team for medical reasons. Retired from active military duty in 1985. Later taught at a Higher School..

1944 June 26 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 18096. FAILURE: Airburst.
  • V-2 M57 G3c - . Nation: Germany. Summary: Airburst 4.7 km to the right of the planned trajectory..

1951 June 26 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1. LV Configuration: R-1 IIIB-5.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1951 June 26 - . 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 June 26 - .
  • Birth of William Arthur Pailes - . Nation: USA. Summary: American engineer military spaceflight engineer astronaut. Flew on STS-51-J..

1953 June 26 - . 19:10 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 38.
  • AF / Utah Ionosphere 3 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 135 km (83 mi). Summary: Ionosphere research. Launched at 1210 local time. Reached 135.2 km..

1954 June 26 - . 13:24 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1D. LV Configuration: R-1D 1.
  • Test / biology / ionosphere / aeronomy mission - . Nation: USSR. Agency: Korolev. Apogee: 106 km (65 mi).

1956 June 26 - .
  • Birth of Dr Bernard Andrew Jr Harris - . Nation: USA. Summary: African-American physician mission specialist astronaut. Flew on STS-55, STS-63. First African-American to walk in space..

1956 June 26 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17. LV Configuration: X-17 D-6A.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 140 km (80 mi). Summary: USAF X-17 flight test program started at Cape Canaveral to study reentry problems by simulating reentry velocities and conditions with three-stage solid-fuel Lockheed X-17. A total of 26 X-17 flights were conducted until March 1957..

1956 June 26 - . 18:26 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee AJ10-34. LV Configuration: Aerobee AJ10-34 USAF 70.
  • E-layer Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 111 km (68 mi). Summary: Ionosphere research. Launched at 1120 local time. Reached 111.1 km..

1957 June 26 - .
  • Birth of Robert Jackson Wood - . Nation: USA. Summary: American physicist payload specialist astronaut, 1985-1986..

1957 June 26 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC9. LV Family: Navaho. Launch Vehicle: Navaho G-26. LV Configuration: Navaho II SM-64 08. FAILURE: One booster engine failed during ascent; did not achieve speed/altitude required for cruise stage ignition.. Failed Stage: 1.
  • Navaho G-26 Flight 4 - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi). The missile launched from the repaired LC-9 on the third attempt. At T+42 seconds, Mach 1.63, and 7,000 m altitude, a fire occurred in the engine compartment after a failure of a regenerative cooling valve to the gas generator. The turbopump shut down, and one engine went out. Nevertheless the vehicle continued, first on one engine, then coasting, to 12,000 m altitude, and the booster separated successfully. But the cruise stage was below ramjet ignition velocity. Again ground control could bring the cruise stage under control as a glider, flying it to an impact 87 km downrange

1957 June 26 - . 11:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC6. LV Family: Redstone. Launch Vehicle: Jupiter A. LV Configuration: Jupiter A CC-31. FAILURE: Human error in calculation of takeoff weight..
  • Jupiter A - . Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Launched at 0609 hours EST from AMR to test performance of the inertial guidance system, angle-of-attack meters, separation of explosive screws, and impact and radar fusing systems. Range instrumentation difficulties and deteriorating weather delayed the firing from the initially scheduled time of 0230 hours EST. The flight was successful. Actual range was 135.425 nm; 0.42 nm over; and 389 meters left of the intended impact point. Missed aimpoint by 785 m.

1958 June 26 - .
  • Materials for thermal protection of satellite reentry vehicles - . Nation: USA. Spacecraft: Mercury. Summary: Meetings were held with NACA, AVCO, and Lockheed representatives in attendance to consider materials for thermal protection of satellite reentry vehicles..

1958 June 26 - . Launch Site: Wallops Island. Launch Vehicle: Exos.
  • Model 1 test - . Nation: USA. Agency: NASA; AFCRL. Apogee: 370 km (220 mi).

1958 June 26 - . 05:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC18A. Launch Pad: LC18A. LV Family: Vanguard. Launch Vehicle: Vanguard. LV Configuration: Vanguard SLV-2. FAILURE: Premature second stage cutoff. Unknown cause.. Failed Stage: 2.
  • Vanguard 2C - . Payload: Lyman Alpha satellite. Mass: 10 kg (22 lb). Nation: USA. Agency: USN. Program: Vanguard. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Vanguard 2. Decay Date: 1958-06-26 . COSPAR: F580626A. Apogee: 165 km (102 mi).

1959 June 26 - . Launch Site: Vandenberg. LV Family: Terrier. Launch Vehicle: Terrier ASROC Cajun. LV Configuration: Terrier ASROC Cajun Terasca.
  • Radar beacon test - . Nation: USA. Agency: USN. Apogee: 100 km (60 mi).

1959 June 26 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC18B. Launch Pad: LC18B. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 198.
  • Series IV research and development launch - . Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).

1960 June 26 - . 06:17 GMT - . Launch Site: Wallops Island. LV Family: Trailblazer. Launch Vehicle: Trailblazer 1. LV Configuration: Trailblazer 1 TB Ib.
  • D58 Trailblazer re-entry vehicle test flight - . Nation: USA. Agency: NASA. Apogee: 294 km (182 mi).

1961 June 26 - . Launch Site: Cape Canaveral. LV Family: Saturn I. Launch Vehicle: Saturn I.
  • Saturn I barge replacement. - . Nation: USA. Program: Apollo. Summary: A Navy YFNB barge was obtained by NASA to serve as a replacement for the Palaemon in transporting of the Saturn booster to Cape Canaveral..

1961 June 26 - . Launch Site: ETR Launch Area. Launch Platform: EAG-154. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2X-11. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1961 June 26 - . 15:15 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.20GT.
  • Attitude control test - . Nation: USA. Agency: NASA. Apogee: 187 km (116 mi).

1962 June 26 - . 08:38 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: HAD. LV Configuration: HAD 108.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 116 km (72 mi).

1962 June 26 - . 10:57 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 21D.
  • NTMP K-1 Target mission - . Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). Summary: First launch of an Atlas from Vandenberg AFB as a target for an Army Nike-Zeus from Kwajalein..

1962 June 26 - . 11:30 GMT - . Launch Site: Kwajalein. LV Family: Nike Zeus. Launch Vehicle: Nike Zeus. LV Configuration: Nike Zeus-3. FAILURE: Failure.
  • First launch of an Army Nike-Zeus from Kwajalein - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi). Summary: First launch of an Army Nike-Zeus from Kwajalein against an Atlas from Vandenberg AFB..

1963 June 26 - .
  • First full-scale firing of the Apollo SM engine - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Electrical. The first full-scale firing of the SM engine was conducted at the Arnold Engineering Development Center. At the start of the shutdown sequence, the engine thrust chamber valve remained open because of an electrical wiring error in the test facility. Consequently the engine ran at a reduced chamber pressure while the propellant in the fuel line was exhausted. During this shutdown transient, the engine's nozzle extension collapsed as a result of excessive pressure differential across the nozzle skin.

1963 June 26 - .
  • Frictionless platform to simulate extravehicular activity - . Nation: USA. Program: Apollo. Spacecraft: A7L. MSC announced that it had contracted with the Martin Company to develop a frictionless platform to simulate the reactions of an extravehicular astronaut in five degrees of freedom-pitch, yaw, roll, forward-backward, and side-to-side. MSC Crew Systems Division would use the simulator to test and evaluate space suits, stabilization devices, tethering lines, and tools.

1964 June 26 - . 00:52 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.157GE.
  • B Field 3 Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 156 km (96 mi).

1965 June 26 - .
  • Poor progress on space trainers - . Nation: USSR. Related Persons: Dementiev; Titov; Smirnov. Program: Voskhod; Lunar L1. Flight: Soyuz 1; Soyuz 2A; Voskhod 3; Voskhod 4; Voskhod 5; Voskhod 6. Spacecraft: Soyuz A; Spiral OS; TMK-E; TMK-1; LK-1. Titov and Kamanin visit LII to review the status of simulator construction. The engineers haven't had any time to even consider trainers for winged spacecraft. The Soyuz trainer will only be completed by July 1966, and the trainer for the new Voskhod configuration is still on paper only. Simulators for manned lunar or planetary flights have not even been discussed yet. It is clear that Kamanin is going to have to go up the chain of command to Dementiev and Smirnov to get resources allocated for the work to be accelerated.

1966 June 26 - . Launch Vehicle: Spiral 50-50.
  • Development of Spiral spaceplane authorised - . Nation: USSR. Spacecraft: Spiral OS; MiG 105-11. Summary: Lozino-Lozinsky was selected as project manager. The Spiral system consisted of three main components: the GSR reusable hypersonic air-breathing launch aircraft; RB expendable two stage rocket; and the OS orbital spaceplane..

1966 June 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC60/7. LV Family: R-16. Launch Vehicle: R-16U.
  • Palma-1 Operational test - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1966 June 26 - . 15:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 147D.
  • NTMP KX-20 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 June 26 - . 21:47 GMT - . Launch Site: Andoya. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache Ferdinand 13.
  • 50 / 70 Hz probe Ionosphere mission - . Nation: Norway. Agency: NDRE. Apogee: 138 km (85 mi).

1967 June 26 - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. FAILURE: Launch vehicle failed to orbit - unknown cause.. Failed Stage: U.
  • Tselina-O GVM - . Payload: Tselina-O Mass Model. Nation: USSR. Agency: RVSN. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-O. COSPAR: F670626A.

1968 June 26 - .
  • State Commission on L1 failure. - . Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1. The State Commission determines the cause of the Proton booster shutdown in April was a short in the L1 abort system. This sent an incorrect abort signal to the launch vehicle, triggering it to shut down its engines. The next L1 launch is set for 19 July, followed by one launch per month thereafter. After 3 or 4 successful unmanned circumlunar missions, the spacecraft will be cleared for a manned lunar flyby.

1968 June 26 - .
  • November manned circumlunar flight set - . Nation: USSR. Program: Lunar L1. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-L1. State commission sets November as date for manned circumlunar flight. The next L1 flight was set for July, with flights to continue at monthly intervals at each translunar launch window. 3 or 4 unmanned flights had to be successful before a manned flight would be attempted.

1968 June 26 - . 04:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 173 km (107 mi).

1968 June 26 - . 09:21 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 168 km (104 mi).

1968 June 26 - . 11:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 229 - . 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: 1968-07-04 . USAF Sat Cat: 3304 . COSPAR: 1968-054A. Apogee: 327 km (203 mi). Perigee: 207 km (128 mi). Inclination: 72.9000 deg. Period: 89.90 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1969 June 26 - . Launch Site: Green River. Launch Complex: Green River Pad 1. LV Family: Athena RTV. Launch Vehicle: Athena RTV. LV Configuration: Athena V142D.
  • USAF V142D re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1969 June 26 - . 18:30 GMT - . Launch Site: Natal. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.53UI.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 795 km (493 mi).

1970 June 26 - .
  • Soyuz 9 crew improving. - . Nation: USSR. Related Persons: Nikolayev; Sevastyanov; Tereshkova. Program: Soyuz. Flight: Soyuz 9. Summary: The Soyuz 9 crew are still suffering from the effects of their flight, but getting better each day. Tereshkova was taken ill last night..

1970 June 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF22. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2559.
  • OT GT59F operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 June 26 - . 03:23 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-14 - . Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1. Decay Date: 1976-02-16 . USAF Sat Cat: 4430 . COSPAR: 1970-049A. Apogee: 39,172 km (24,340 mi). Perigee: 459 km (285 mi). Inclination: 65.5000 deg. Period: 703.10 min. Summary: Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network..

1970 June 26 - . 12:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 350 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 12.00 days. Decay Date: 1970-07-08 . USAF Sat Cat: 4425 . COSPAR: 1970-050A. Apogee: 274 km (170 mi). Perigee: 180 km (110 mi). Inclination: 51.7000 deg. Period: 89.00 min. Summary: Area survey photo reconnaissance satellite; returned film capsule..

1970 June 26 - . 18:20 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Apogee: 145 km (90 mi).

1971 June 26 - .
  • Soyuz 11 Day 21 - . Nation: USSR. Related Persons: Dobrovolsky; Patsayev; Volkov. Program: Salyut. Flight: Soyuz 11. Spacecraft: Soyuz 7KT-OK; Salyut 1. The crew has completed all scientific and technical experiments aboard the Salyut station. They will spend the last two to three days concentrating on physical training, medical observations, and preparation for landing. They will turn off all station equipment not required for autonomous flight, prepare the Soyuz for landing, and measure the water and consumable reserves available for the next crew. The experiments have produced many film cartridges, experiment samples, and so on that should be returned to earth. However there is not enough space or mass reserves in the Soyuz capsule for them all so they are only to return those specifically listed by ground control.

1971 June 26 - . Launch Site: Biscarosse. Launch Platform: S611. LV Family: MSBS. Launch Vehicle: MSBS M1.
  • Operational test - . Nation: France. Agency: DMA. Apogee: 500 km (310 mi).

1971 June 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC142/34. LV Family: Tsiklon. Launch Vehicle: R-36 8K67M.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1971 June 26 - . 19:44 GMT - . Launch Site: South Uist. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P120H.
  • Solar La / X / ne Ionosphere / solar extreme ultraviolet mission - . Nation: UK. Agency: SRC. Apogee: 143 km (88 mi).

1971 June 26 - . 23:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC110L. LV Family: N1. Launch Vehicle: N1. LV Configuration: N-1 11A52 6L. FAILURE: First stage failed.. Failed Stage: 1.
  • N1 6L - . Payload: Soyuz 7K-LOK / LK Mockups. Nation: USSR. Agency: RVSN. Program: Lunar L3. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-LOK. Decay Date: 1971-07-21 . COSPAR: F710626A. Apogee: 1.00 km (0.60 mi). Superbooster failure of N1 serial number 6L. This was a substantially improved vehicle, incorporating filters in the propellant lines to prevent any foreign objects from getting into the pumps. The shape of the tail of the booster was modified, and ventilation and refrigeration systems were added to keep the engine compartment cool. It was painted white overall to reduce temperatures while sitting on the pad. After liftoff and ascent, an axial rotation was introduced by gas dynamics interactions of the thirty engines with the air slipstream. The launch vehicle developed a roll beyond the capability of the control system to compensate. and began to break up as it went through Max Q. Control was lost at 50.2 seconds into the flight and it was destroyed by range safety a second later. The engines functioned well and did not shut down up to the point of vehicle destruction. No functional payload was carried. It has been stated that this launch did not have a working launch escape system. Additional Details: N1 6L.

1972 June 26 - .
  • No foreseeable mission for Apollo Apollo CSMs 115 and 115a - . Nation: USA. Related Persons: Low, George. Program: Apollo. Spacecraft: Apollo CSM; CSM Block II. NASA Deputy Administrator George M. Low and Associate Administrator for Manned Space Flight Dale D. Myers met and decided there was no foreseeable mission for CSMs 115 and 115a; funds would not be authorized for any work on these spacecraft; and skills would not be retained specifically to work on them.

1972 June 26 - .
  • AUOS satellite development approved. - . Nation: USSR. Spacecraft: AUOS. Summary: Ministry of General Machine Building (MOM) Decree 'On the Creation of Automatic Universal Orbital Stations (AUOS)-on approval of work on the AUOS satellite bus' was issued..

1972 June 26 - . 14:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511.
  • Cosmos 496 - . Payload: Soyuz 7K-T s/n 33L. Mass: 6,675 kg (14,715 lb). Nation: USSR. Agency: MOM. Program: Salyut. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-T. Duration: 9.95 days. Decay Date: 1972-07-02 . USAF Sat Cat: 6066 . COSPAR: 1972-045A. Apogee: 253 km (157 mi). Perigee: 176 km (109 mi). Inclination: 51.5000 deg. Period: 88.70 min. Summary: Recovered July 6, 1972 13:54 GMT. Soyuz 7K-T redesign test..

1973 June 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 24B. LV Configuration: Titan 24B 24B-9 (3B-43). FAILURE: Agena upper stage failed to orbit.. Failed Stage: 3.
  • OPS 4018 - . Payload: KH-8 no. 39 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-8. Decay Date: 1973-06-26 . COSPAR: F730626AA.

1973 June 26 - . 01:22 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu47121-16. FAILURE: Nine persons were killed in the explosion of the vehicle.. Failed Stage: U.
  • Nine killed in fuelling accident at Plesetsk - . Nation: USSR. Agency: RVSN. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-O. COSPAR: F730626BA. Summary: Nine were killed at the LC-133 Voskhod complex during preparation of a Kosmos-3M booster. Oxidiser and propellant were accidentally mixed together during fuelling..

1973 June 26 - . 17:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 24B. LV Configuration: Titan 24B 3B-43 (24B-9). FAILURE: Failure.
  • SRV-1 - . Nation: USA. Agency: USAF. Spacecraft: KH-8. COSPAR: F730626AC.
  • SRV-2 - . Nation: USA. Agency: USAF. Spacecraft: KH-8. COSPAR: F730626AD.

1974 June 26 - . 12:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 662 - . Payload: DS-P1-I s/n 14. Mass: 400 kg (880 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-I. Completed Operations Date: 1975-03-17 . Decay Date: 1976-08-28 . USAF Sat Cat: 7347 . COSPAR: 1974-047A. Apogee: 812 km (504 mi). Perigee: 271 km (168 mi). Inclination: 70.9000 deg. Period: 95.50 min. Summary: Operational radar target for the ABM forces..

1975 June 26 - . 16:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHOK. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1976 June 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).

1976 June 26 - . 03:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 23C-10 (3C-28).
  • IMEWS 6 - . Payload: DSP Phase 2 s/n 8 / OPS 2112. Mass: 1,040 kg (2,290 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: DSP. Completed Operations Date: 1984-07-01 . USAF Sat Cat: 8916 . COSPAR: 1976-059A. Apogee: 35,860 km (22,280 mi). Perigee: 35,620 km (22,130 mi). Inclination: 0.5000 deg. Period: 1,433.30 min. Second generation geosynchronous ballistic missile launch detection satellite, remained in service for over eight years. Positioned over the Atlantic Ocean from 1976 to 1981: at 35 deg W in 1976-1977; at 65 deg W in 1977-1979; and 35 deg W in 1979-1980; and 65 deg W in 1980-1981. Then moved over the Pacific Ocean at 125 deg W, then 140 deg W in 1981-1982; then over the Indian Ocean at 75 deg E in 1982-1984.

1976 June 26 - . 08:58 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 640. Launch Vehicle: Poseidon.
  • FOT-21? Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1976 June 26 - . 09:06 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 640. Launch Vehicle: Poseidon.
  • FOT-21? Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1977 June 26 - . Launch Site: Vandenberg.
  • Final launch of an Atlas/Agena booster/upper stage - . Nation: USA. Summary: Final launch of an Atlas/Agena booster/upper stage combination from Vandenberg AFB (first launch on 11 October 1 960)..

1978 June 26 - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1019CE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 315 km (195 mi).

1978 June 26 - . 20:31 GMT - . Launch Site: Wallops Island. Launch Platform: VISE. LV Family: MR-12. Launch Vehicle: MR-12. LV Configuration: MR-12 D-75MG.
  • JASPIC - . Nation: USSR. Apogee: 165 km (102 mi).

1979 June 26 - . Launch Site: Baikonur. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100U 15A16.
  • SLI? - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1980 June 26 - . 12:20 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1189 - . 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: 1980-07-10 . USAF Sat Cat: 11863 . COSPAR: 1980-054A. Apogee: 305 km (189 mi). Perigee: 198 km (123 mi). Inclination: 72.9000 deg. Period: 89.60 min. Summary: Photo surveillance; returned film capsule; maneuverable..

1981 June 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT83GB Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1982 June 26 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 620. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1982 June 26 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S3. LV Configuration: SSBS S3 2605.
  • Operational test - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1982 June 26 - . 02:57 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 620. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1984 June 26 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle Discovery Pad Abort - . Nation: USA. Program: STS. Flight: STS-41-D. Spacecraft: Discovery. Summary: The countdown for the second launch attempt for Discovery's maiden flight ended at T- 4 seconds when the orbiter's computers detected a sluggish valve in main engine #3. The main engine was replaced and Discovery was finally launched on August 30, 1984..

1984 June 26 - . 15:35 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1576 - . 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: 1984-08-24 . USAF Sat Cat: 15070 . COSPAR: 1984-066A. Apogee: 348 km (216 mi). Perigee: 167 km (103 mi). Inclination: 67.1000 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..

1985 June 26 - . 12:35 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1664 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 9.00 days. Decay Date: 1985-07-05 . USAF Sat Cat: 15860 . COSPAR: 1985-054A. Apogee: 376 km (233 mi). Perigee: 193 km (119 mi). Inclination: 72.8000 deg. Period: 90.20 min. Summary: Military cartographic satellite; returned film capsule; maneuverable..

1985 June 26 - . 17:46 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.54UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1986 June 26 - . 13:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Pershing. Launch Vehicle: Pershing 2.
  • Operational test - . Nation: USA. Agency: USA. Apogee: 250 km (150 mi).

1987 June 26 - . 07:01 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: KRENKEL'. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 59 km (36 mi).

1988 June 26 - . Launch Site: Thumba. LV Family: RH. Launch Vehicle: RH-200.
  • Meteorological Chaff Meteorological mission - . Nation: India. Agency: ISRO. Apogee: 70 km (43 mi).

1989 June 26 - . 09:20 GMT - . Launch Site: Sea-launched. Launch Pad: SAIN. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1990 June 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT140GB Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1991 June 26 - . 02:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT144GB Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1992 June 26 - . 18:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 70 km (43 mi).

1993 June 26 - . 13:27 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 D221.
  • USA 92 - . Payload: GPS 2A-21 / GPS SVN 39. Mass: 1,816 kg (4,003 lb). Nation: USA. Agency: USAF. Manufacturer: Seal Beach. Program: Navstar. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2 and 2A. USAF Sat Cat: 22700 . COSPAR: 1993-042A. Apogee: 20,250 km (12,580 mi). Perigee: 20,112 km (12,496 mi). Inclination: 54.6000 deg. Period: 717.90 min. Summary: Global Positioning System. Placed in Plane A Slot 1..
  • PMG Far End Package - . Nation: USA. Agency: MDSSC. Program: Navstar. Spacecraft: PMG. COSPAR: 1993-042xx.
  • PMG - . Payload: Plasma Motor Generator. Nation: USA. Agency: MDAC. Program: Navstar. Spacecraft: PMG. Decay Date: 1993-08-30 . USAF Sat Cat: 22701 . COSPAR: 1993-042B. Apogee: 677 km (420 mi). Perigee: 185 km (114 mi). Inclination: 25.7000 deg. Period: 93.20 min.

1995 June 26 - . Launch Site: Barking Sands. LV Family: Strypi. Launch Vehicle: Strypi IX. FAILURE: Failure.
  • ETCE-11 Target mission - . Nation: USA. Agency: USA SMDC. Apogee: 200 km (120 mi).

1996 June 26 - . 12:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF10. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT162GM.
  • FOT GT162GM Follow-on Test launch - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

1996 June 26 - . 14:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT160GM.
  • FOT GT160GM Follow-on Test launch - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

1996 June 26 - . 19:00 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 36.147US.
  • USC-1 SOHO Cal Solar extreme ultraviolet mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 309 km (192 mi).

1997 June 26 - .
  • Mir News 363: The following message received from VideoCosmos - . Nation: Russia. Program: Mir. Flight: Mir NASA-4; Mir EO-23. Co redistributed by Chris v.d.Berg under MirNEWS.363 and MirNWS.363 (no Dutch translation available yet due to lack of time)

    Subject: Emergency on Mir

    Novosti Kosmonavtiki June 25, 1997 -- Moscow, Russia -- Progress M-34 cargo vehicle collided With the Spektr module of Mir space station earlier today but the crew survived. The collision occurred before 09:18 UTC during Progress' fly around in remote control mode before scheduled re-docking. The crew haven't had communications with Russian ground stations at the time. The cargo spacecraft sheared a half of Spektr solar panel and made damage to the module itself. Depressurization of the station had begun but the crew succeeded in fast closing the hatch to Spektr. The rest of the station is being re-pressurised. Also, thermal control radiators on Spektr were damaged. There is no immediate danger to the crew but emergency landing is a possible decision. This report is not copyrighted. If you plan to use or publish the report please keep reference to VideoCosmos Co. of Moscow, Russia, and Novosti Kosmonavtiki Magazine.

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


2001 June 26 - .
  • Death of John Finley Yardley - . Nation: USA. Related Persons: Yardley. Summary: American engineer. Headed the Mercury, Gemini, and Skylab programs at McDonnell; led development of the space shuttle through its first flight at NASA..

2002 June 26 - . 05:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Progress M-46 - . Payload: Progress M s/n 246. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-5. Spacecraft: Progress M. Duration: 110.00 days. Decay Date: 2002-10-14 . USAF Sat Cat: 27454 . COSPAR: 2002-033A. Apogee: 397 km (246 mi). Perigee: 387 km (240 mi). Inclination: 51.6000 deg. Period: 92.40 min. Launch delayed from May 21, then moved forward from July 14. Progress M-46 was launched on ISS mission 8P and docked with the Zvezda module at 0623 UTC on June 29 after carrying out tests of the Kurs rendezvous system on June 28. Seperated from ISS and commanded to destructive re-entry on 14 October 2002.

2003 June 26 - . 18:55 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F34.
  • Orbview 3 - . Mass: 304 kg (670 lb). Nation: USA. Agency: McLean. Program: Orbview. Class: Earth. Type: Earth resources satellite. Spacecraft: Orbview. Decay Date: 2011-03-13 . USAF Sat Cat: 27838 . COSPAR: 2003-030A. Apogee: 455 km (282 mi). Perigee: 452 km (280 mi). Inclination: 97.3000 deg. Period: 93.70 min. One-meter-resolution commercial imaging satellite. Orbview-3 used an Orbital Leostar bus and had a launch mass of 304 kg (including ca. 50 kg of hydrazine for orbit raising and the 66 kg science instrument). Launch had been delayed from September 2002, April 30, May 9 and 23

2006 June 26 - .
2007 June 26 - . Launch Site: White Sands. Launch Vehicle: THAAD.
  • Low Endo - . Nation: USA. Agency: USA. Apogee: 40 km (24 mi).

2008 June 26 - .
  • ISS On-Orbit Status 06/26/08 - . Nation: USA. Related Persons: Kononenko, O D; Love; Nyberg; Volkov, Sergey. Program: ISS. Flight: ISS EO-17; STS-122; STS-124. Today at ~9:55am EDT, the ISS (specifically its FGB module) completed 55,000 orbits of the Earth, having covered a distance of 2.

    2 billion kilometers (1.45 billion st.miles) in 3506 days. The 19,300 kg (42,600 lbs) Zarya ('Dawn') was launched on a Russian/Khrunichev Proton from Baikonur over 9.5 years ago (11/20/98) as the first element of the multi-national space station.<<<<

    Current sleep cycle: Crew wakeup last night: 11:00pm EDT; sleeptime today: 3:30pm. Wakeup tomorrow: back at 2:00am, for a half-duty day.

    Crew activities focused on a thorough Orlan systems checkout and suited exercise in preparation for the EVA-20a on 7/10. The successful Orlan-suited dry run demonstrated that in the case of a contingency situation during the spacewalk, the crew would be able to ingress the Soyuz module while still in their Orlan suits. The activities were recorded on VTR (Video Tape Recorder) by camcorder equipment set up by FE-2 Chamitoff. (Plans for live TV downlink during the run had to be scrapped because a necessary drag-through cable could not be located in time.) Additional Details: ISS On-Orbit Status 06/26/08.


2009 June 26 - . 09:30 GMT - . Launch Site: Wallops Island. LV Family: Terrier. Launch Vehicle: Terrier Orion.
  • NASA 41.083UO - . Nation: USA. Agency: NASA Greenbelt. Apogee: 117 km (72 mi). Summary: Education.

2010 June 26 - . 21:41 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.
  • Coms 1 - . Mass: 2,400 kg (5,200 lb). Nation: Korea South. Agency: Arianespace. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36744 . COSPAR: 2010-032A. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Communication, Ocean and Meteorological Satellite. Weather, oceanography, and communications payloads..
  • Arabsat 5A - . Mass: 4,800 kg (10,500 lb). Nation: Arab States. Agency: Arianespace. Program: Arabsat. Class: Communications. Type: Communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 36745 . COSPAR: 2010-032B. Apogee: 35,789 km (22,238 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Communications satellite with 16 C-band and 24 Ku-band transponders, stationed at 30.5 deg E..

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