On June 29 in Space History
Chronology
114 events
1933 June 29
Launch Site: Magdeburg. Launch Vehicle: Magdeburg.- Magdeburg launch - .
Nation: Germany.
Apogee: 0.0100 km (0.0062 mi). Range: 0.31 km (0.19 mi).
The 200 kgf prototype rocket is finally launched. However it catches on one of the rails in the launch tower and is flung horizontally as it clears the tower. It flies 300 m horizontally over the pastures, then slides along the ground for 10 m more. It is relatively intact, but the Magdeburg city officials are not interested in funding further attempts. Nebel receives only 3200 Marks for his work.
1943 June 29
Launch Site: Peenemuende. Launch Complex: Peenemuende. Launch Vehicle: V-2.- Himmler's second visit to Peenemuende - .
Nation: Germany.
The rocket team and SS entourage discussed politics until 4 am. The next morning, the first demonstration launch of a V-2 failed - the missile turned west at an altitude of 200 m, and crashed in the woods outside of Peenmuende-West, destroying three aircraft on the nearby runway. Fortunately no one was killed. The second launch in the afternoon was successful. But the bureaucratic efforts by the SS and other organisations to take over the rocket program from the Army continued.
1943 June 29
Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. FAILURE: Fell on airstrip. Range 3 km.1943 June 29
Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2.1951 June 29
Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: MGR-1.- Test mission - . Nation: USA. Apogee: 10 km (6 mi).
1955 June 29
- Birth of Charles Joseph 'Charlie' Precourt - . Nation: USA. Related Persons: Precourt. American test pilot astronaut 1990-2005. 4 spaceflights, 38.8 days in space. Flew to orbit on STS-55 (1993), STS-71, STS-84, STS-91..
1956 June 29
19:09 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee Hi.- RV-N-13b Ionosphere mission - . Nation: USA. Agency: NRL. Apogee: 264 km (164 mi). Ionosphere research. Launched at 1200 local time. Reached 261 km..
1957 June 29
Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar SP-2. LV Family: V-2. Launch Vehicle: R-2A.- NIIP-A target - . Nation: Russia. Agency: Korolev bureau. Apogee: 100 km (60 mi).
1959 June 29
Launch Site: Aberporth. Launch Vehicle: Rook. FAILURE: Failure.- Test mission - . Nation: UK. Agency: Royal Aerospace Establishment. Apogee: 0 km (0 mi).
1959 June 29
11:33 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA5A. Launch Vehicle: Black Knight.- Research and development launch - . Nation: UK. Agency: Royal Aerospace Establishment. Apogee: 442 km (274 mi).
1959 June 29
15:42 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25A. LV Family: Polaris. Launch Vehicle: Polaris AX.1960 June 29
22:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1W. LV Family: Thor. Launch Vehicle: Thor Agena A. FAILURE: Failure. Failed Stage: U.- Discoverer 12 - . Payload: KH-1 prototype. Mass: 790 kg (1,740 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: WS-117. Spacecraft: KH-1. Decay Date: 1960-06-29 . KH-1 prototype; designed to test capsule recovery system; did not carry camera..
- SRV - . Mass: 779 kg (1,717 lb). Nation: USA. Agency: USAF. Spacecraft Bus: WS-117. Spacecraft: KH-1.
1961 June 29
04:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Ablestar.- Transit 4A - . Mass: 79 kg (174 lb). Nation: USA. Agency: USN. Program: Transit. Class: Navigation. Type: Navigation satellite. Spacecraft: Transit. USAF Sat Cat: 116 . COSPAR: 1961-Omicron-1. Apogee: 986 km (612 mi). Perigee: 865 km (537 mi). Inclination: 66.80 deg. Period: 103.50 min. Transits 4A and 4B were drum-shaped instead of spherical to provide more space for solar cells. In addition, operational 150-and 400-MHz frequencies were used for the first time. Carried SNAP-3A nuclear power source..
- Solrad 3 - . Payload: Grab 2. Mass: 18 kg (39 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: SIGINT. Spacecraft: GRAB. COSPAR: 1961-Omicron-xx. ELINT satellite, retransmitting to US ground stations signals from Soviet radar stations. Classified at time; official purpose and secondary payload collected solar radiation data..
- Injun 1 - . Mass: 25 kg (55 lb). Nation: USA. Agency: USN. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Injun. USAF Sat Cat: 117 . COSPAR: 1961-Omicron-2. Apogee: 992 km (616 mi). Perigee: 869 km (539 mi). Inclination: 66.80 deg. Period: 103.60 min. Dual launch; failed to separate from Solrad 3; still returned radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1962 June 29
- Birth of George David 'Zambo' Zamka - . Nation: USA. Related Persons: Zamka. American test pilot astronaut 1998-2011. Grew up in Rochester, Michigan. US Marine Corps. 2 spaceflights, 28.9 days in space. Flew to orbit on STS-120 (2007), STS-130..
1962 June 29
05:40 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1A.- Research and development test - . Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). First Air Force crew launch.
1962 June 29
14:06 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25A. LV Family: Polaris. Launch Vehicle: Polaris A2.1962 June 29
18:41 GMT - . Launch Site: Edwards. Launch Complex: Hidden Hills DZ. Launch Pad: Edwards RW04/22. Launch Platform: NB-52 008.- X-15A Heating rates, notch test - . Nation: USA. Agency: NASA, USAF. Spacecraft: X-15A. Apogee: 25 km (15 mi). Maximum Speed - 5278 kph. Maximum Altitude - 25360 m. Air dropped in Hidden Hills DZ..
1962 June 29
21:00 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A.1963 June 29
- Vostok 5/6 cosmonauts preparared for first international press conference. - .
Nation: Russia.
Related Persons: Bykovsky,
Keldysh,
Serbin,
Tereshkova.
Flight: Vostok 5,
Vostok 6.
Spacecraft: Vostok.
At a meeting of the Central Committee, Tereshkova and Bykovskiy are taken through possible questions and correct replies by Serbin and Keldysh in preparation for their first international press conference. The training extends form 10 in the morning to 17:00 in the afternoon.
1963 June 29
16:46 GMT - . Launch Site: Eglin. LV Family: Aerobee. Launch Vehicle: Aerobee 150.1963 June 29
22:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Thor. Launch Vehicle: Thor SLV-2A Agena B.- OPS 1440 - .
Payload: Ferret 4 / Agena B 2314. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-10-26 . USAF Sat Cat: 613 . COSPAR: 1963-027A. Apogee: 530 km (320 mi). Perigee: 487 km (302 mi). Inclination: 82.30 deg. Period: 94.80 min.
An Air Force Thor/Agena B launched from Vandenberg established a number of distinctive records. It was the 200th Thor to be launched since Number 101 was launched at Cape Canaveral on 25 January 1957. It was the first, last and only-Thrust Augmented Thor/Agena B to be used by the Air Force. It was the final Agena B (#2314) to be employed with a Thor booster.
1964 June 29
Launch Site: Jiuquan. Launch Complex: Jiuquan LA3. LV Family: R-12. Launch Vehicle: DF-2.- Nation: China. Agency: PRC. Apogee: 200 km (120 mi). This followed a two-year complete redesign and test program following the first launch failure in 1962. The reduced-thrust missile had a range of 1050 km with a 1550 kg warhead, barely enough to reach Japan..
1964 June 29
21:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.1965 June 29
- Apollo PA-2 launch escape system test - .
Nation: USA.
Program: Apollo.
Spacecraft: Apollo CSM,
CSM LES,
CSM Recovery.
NASA launched Apollo mission PA-2, a test of the launch escape system (LES) simulating a pad abort at WSMR. All test objectives were met. The escape rocket lifted the spacecraft (boilerplate 23A) more than 1,524 m (5,000 ft) above the pad. The earth landing system functioned normally, lowering the vehicle back to earth. This flight was similar to the first pad abort test on November 7, 1963, except for the addition of canards to the LES (to orient the spacecraft blunt end forward after engine burnout) and a boost protective cover on the CM. PA-2 was the fifth of six scheduled flights to prove out the LES.
1965 June 29
Launch Site: Baikonur. Launch Complex: Baikonur LC60/7. LV Family: R-16. Launch Vehicle: R-16U. FAILURE: Failure.1965 June 29
Launch Site: Eglin. LV Family: Hydac. Launch Vehicle: Nike Javelin.1965 June 29
12:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.1965 June 29
13:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Apollo CSM. Launch Vehicle: Apollo LES.1965 June 29
17:45 GMT - . Launch Site: Eglin. LV Family: Hydac. Launch Vehicle: HJ Nike Javelin.1965 June 29
18:21 GMT - . Launch Site: Edwards. Launch Complex: Delamar Dry Lake DZ. Launch Pad: Edwards RW04/22. Launch Platform: NB-52 008.- X-15A LaRC Scan,Radiom,BLN Test/Aeronomy mission - . Nation: USA. Agency: NASA, USAF. Spacecraft: X-15A. Apogee: 85 km (52 mi). Maximum Speed - 5522 kph. Maximum Altitude - 85527 m. Astronaut wings flight (USAF definition). Air dropped in Delamar Dry Lake DZ..
1965 June 29
19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150.1966 June 29
Launch Site: Vandenberg. Launch Complex: Vandenberg. LV Family: Titan. Launch Vehicle: Titan IIIB.- Initial launch of a satellite by Titan IIIB/Agena - . Nation: USA. Nation's initial launch of a satellite by a Titan IIIB/Agena space booster (first launch of a Titan III from Vandenberg AFB)..
1966 June 29
Launch Site: Gilson Butte. LV Family: Pershing. Launch Vehicle: Pershing 1.1967 June 29
Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.1967 June 29
18:27 GMT - . Launch Site: Edwards. Launch Complex: Smith Ranch Lake DZ. Launch Pad: Edwards RW04/22. Launch Platform: NB-52 008. FAILURE: Loss of both APU's and all electrical power..- X-15A WTR/HS/ASAS Test/Technology mission - . Nation: USA. Agency: NASA, USAF. Spacecraft: X-15A. Apogee: 52 km (32 mi). Electrical failure while climbing through 32610 m; lost engine at 69 seconds; landed at Mud Lake with no flaps; Knight injured while exiting aircraft. Maximum Speed - 4618 kph. Maximum Altitude - 52730 m. Air dropped in Smith Ranch Lake DZ..
1967 June 29
21:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10W. LV Family: Thor. Launch Vehicle: Thor Burner 2.- SECOR 9 - .
Payload: EGRS 9. Mass: 20 kg (44 lb). Nation: USA.
Agency: USA ACE.
Class: Earth.
Type: Geodetic satellite. Spacecraft: SECOR.
USAF Sat Cat: 2861 . COSPAR: 1967-065A. Apogee: 3,940 km (2,440 mi). Perigee: 3,803 km (2,363 mi). Inclination: 90.20 deg. Period: 172.10 min.
Two scientific satellites, an Army Sequential Collation of Range (SECOR) and a Navy Aurora I, were launched from Vandenberg aboard a Thor/Burner II. This was the first flight in the Department of Defense's Space Experiments Support Program (SESP), a tri-service program that allowed qualified government-sponsored space experimenters to fly payloads on Air Force boosters. Space Systems Division managed the program and provided boosters, payload integration, and launch services. Defense's Space Experiments Support Program (SESP), a tri-service program that allowed qualified government-sponsored space experimenters to fly payloads on Air Force boosters. Space Systems Division managed the program and provided boosters, payload integration, and launch services. Location survey. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- Aurora 1 - .
Payload: Aurora (P 67-1). Mass: 21 kg (46 lb). Nation: USA.
Agency: USN.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Aurora.
USAF Sat Cat: 2876 . COSPAR: 1967-065B. Apogee: 3,937 km (2,446 mi). Perigee: 3,808 km (2,366 mi). Inclination: 90.20 deg. Period: 172.10 min.
Two scientific satellites, an Army Sequential Collation of Range (SECOR) and a Navy Aurora I, were launched from Vandenberg aboard a Thor/Burner II. This was the first flight in the Department of Defense's Space Experiments Support Program (SESP), a tri-service program that allowed qualified government-sponsored space experimenters to fly payloads on Air Force boosters. Space Systems Division managed the program and provided boosters, payload integration, and launch services. Defense's Space Experiments Support Program (SESP), a tri-service program that allowed qualified government-sponsored space experimenters to fly payloads on Air Force boosters. Space Systems Division managed the program and provided boosters, payload integration, and launch services. Investigated aurora borealis. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1968 June 29
Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F.- ABRES RVTO-1A-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Spacecraft: ABRES. Apogee: 1,400 km (800 mi).
1969 June 29
03:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Thor Delta N.- Biosatellite 3 - .
Payload: Biosat 3. Mass: 695 kg (1,532 lb). Nation: USA.
Agency: NASA Ames.
Class: Biology.
Type: Biology satellite. Spacecraft: Biosatellite.
Decay Date: 1970-01-20 . USAF Sat Cat: 4000 . COSPAR: 1969-056A. Apogee: 374 km (232 mi). Perigee: 363 km (225 mi). Inclination: 33.50 deg. Period: 92.00 min.
Biological capsule reentered 7/7/69. The intent had been to fly a 6 kg male pig-tailed monkey (Macaca nemestrina) named Bonnie in Earth-orbit for 30 days. However, after only 8.8 days in orbit, the mission was terminated because of the subject's deteriorating health. High development costs were a strong incentive for maximising the scientific return from the mission. Because of this, the scientific goals had become exceedingly ambitious over time, and a great many measurements were conducted on the single research subject flown. Although the mission was highly successful from a technical standpoint, the science results were apparently compromised. Additional Details: here....
1970 June 29
- Additional Soyuz flights requested. - . Nation: Russia. Related Persons: Kutakhov. Program: Soyuz. Flight: Soyuz 9. Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-OK. Kamanin pleads with Kutakhov for construction of at least 3 to 4 new Soyuz spacecraft, and necessary improvements to Star City facilities..
1970 June 29
Launch Site: Baikonur. Launch Complex: Baikonur LC162/36. LV Family: R-36. Launch Vehicle: R-36 8K67.1970 June 29
Launch Site: Plesetsk. LV Family: RT-2. Launch Vehicle: RT-2P.1971 June 29
- Soyuz 11 day 24 - final preparations for landing. - .
Nation: Russia.
Related Persons: Dobrovolsky,
Mishin,
Patsayev,
Volkov,
Yeliseyev.
Program: Salyut,
Lunar L3.
Flight: Soyuz 11.
Spacecraft: Salyut 1,
Soyuz 7KT-OK.
Big dramas are being played out at the cosmodrome over the N1 failure, but Mishin seems protected by someone very high up and is untouchable in the blame game. This is the last full day aloft of the Soyuz 11 crew. At 19:30 the State Commission at the command point authorises the Soyuz 11 crew to undock from the Salyut space station. A communications session begins on the 15th orbit of the day at 19:45. Dobrovolsky and Volkov confirmed that the station was completely mothballed, all material to be returned was stowed in the Soyuz capsule, the crew was wearing their anti-G suits, and had completed shut-down of the station. Yeliseyev advised the crew that ground telemetry showed that they had not turned on the noxious gas filters in the station. Volkov argues that this must be a ground control error, but after checking admits the crew made a mistake.
After the crew has left the station, taken their seats in the capsule, and closed the hatch between the Soyuz BO orbital module and SA re-entry capsule, the strained voice of Volkov comes from space: 'Hatch not hermetically sealed? What's happening? What's going on?'. All this response to the fact that the caution and warning panel 'Hatch open' light has not gone out. Yeliseyev calmly advises the crew, 'Don't panic. Open the hatch, and move the wheel to the left to open. Close the hatch, and then move the wheel to the right six turns with full force'. The crew does this several times, but the light still won't go out. On a final attempt, with 6.5 turns of the wheel, the light goes out. On the second half of he 15th orbit, the crew lowers the pressure in the BO to 160 mm, and the hatch proves to be air-tight.
On the 16th orbit the crew separates their Soyuz from the Salyut station. At 21:35 they report normal separation and that they 'can see how the station moves away from the spacecraft'. They have enough propellant to stop the separation velocity, and take photographs of the station from 10 to 15 m away. They then back away to 30-40 m, and Patsayev takes another set of photographs documenting the condition of the station.
1971 June 29
Launch Site: , Vandenberg.- Four missile launches from Vandenberg in a single day. - . The Space and Missile Test Center (SAMTEC) equalled its previous record by supporting four missile launches from Vandenberg in a single day..
1971 June 29
Launch Site: Plesetsk. LV Family: R-16. Launch Vehicle: R-16U.1971 June 29
09:10 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170.1971 June 29
13:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg PLC-C. LV Family: Aerobee. Launch Vehicle: Aerobee 170.- CHASER 1 ABM infrared sensor technology mission - . Nation: USA. Agency: USAF AFSC. Apogee: 161 km (100 mi).
1971 June 29
13:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas F/Trident.- ABRES RVTO-2A-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Spacecraft: ABRES. Apogee: 1,400 km (800 mi).
1971 June 29
- Landing of Soyuz 11 - .
Return Crew: Dobrovolsky,
Patsayev,
Volkov.
Nation: Russia.
Related Persons: Dobrovolsky,
Patsayev,
Volkov.
Program: Salyut.
Flight: Soyuz 11.
The re-entry capsule was recovered June 29, 1971 23:17 GMT, but when the hatch was opened it was found that the crew had perished due to a loss of cabin atmosphere. A pressure equalization valve was jerked loose at the jettison of the Soyuz Orbital Module. The valve was not supposed to open until an altitude of 4 km was reached. The three-man crew did not have space suits. The Soyuz was thereafter redesigned to accomodate only two crew, but in spacesuits. The actual Soyuz 11 Prime Crew was Leonov, Kubasov, and Kolodin. Dobrovolskiy, Volkov, Patsayev were their backups (and support crew to Soyuz 10). Kubasov was grounded by physicians few days before launch, and the back-up crew ended up going instead.
1972 June 29
Launch Site: Yurya. LV Family: R-16. Launch Vehicle: R-16U.1972 June 29
03:47 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.- Prognoz 2 - . Payload: SO-M no. 2. Mass: 845 kg (1,862 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Prognoz. Decay Date: 1982-12-15 . USAF Sat Cat: 6068 . COSPAR: 1972-046A. Apogee: 201,804 km (125,394 mi). Perigee: 517 km (321 mi). Inclination: 65.30 deg. Period: 5,849.20 min. Study of the processes of solar activity and of their influence on interplanetary space and the Earth's magnetosphere. .
1973 June 29
Launch Site: Malmstrom AFB. LV Family: Minuteman. Launch Vehicle: Minuteman 2.- Malmstrom AFB - . Air Force Logistics Command (AFLC) completed the Minuteman II Balance of Force Retrofit program at Wing I, Malmstrom AFB, Montana..
1973 June 29
Launch Site: Kheysa. Launch Vehicle: MR-12.1973 June 29
11:59 GMT - . Launch Site: South Uist. Launch Vehicle: Petrel.1974 June 29
01:10 GMT - . Launch Site: Wallops Island. Launch Vehicle: Nike Iroquois.- Aladdin 74 Pre-Aladdin Aeronomy / Chemical release mission - . Nation: USA. Agency: USAF CRL. Apogee: 184 km (114 mi).
1974 June 29
12:50 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511M.- Cosmos 664 - . Mass: 6,000 kg (13,200 lb). Nation: Russia. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: Vostok. Spacecraft: Zenit-4MT. Duration: 12.00 days. Decay Date: 1974-07-11 . USAF Sat Cat: 7351 . COSPAR: 1974-049A. Apogee: 341 km (211 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 90.00 min. Military topography satellite; returned film capsule; separated science capsule..
1974 June 29
15:59 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Molniya 8K78M.- Cosmos 665 - . Payload: Oko #3. Mass: 1,250 kg (2,750 lb). Nation: Russia. Agency: MOM. Class: Surveillance. Type: Early warning satellite. Spacecraft: Oko. Decay Date: 1990-07-06 . USAF Sat Cat: 7352 . COSPAR: 1974-050A. Apogee: 39,653 km (24,639 mi). Perigee: 298 km (185 mi). Inclination: 61.80 deg. Period: 709.60 min. Covered Oko constellation plane 2 - 315 degree longitude of ascending node..
1974 June 29
19:45 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 170.- Aladdin 74 extreme ultraviolet Airglow Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 211 km (131 mi).
1974 June 29
20:00 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk. Launch Vehicle: Ute Tomahawk.- Aladdin 74 NMS / E Aeronomy / plasma mission - . Nation: USA. Agency: USAF CRL. Apogee: 110 km (60 mi).
1974 June 29
20:16 GMT - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant VC.1974 June 29
20:33 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk. Launch Vehicle: Nike Tomahawk.1974 June 29
21:05 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk. Launch Vehicle: Nike Tomahawk.1974 June 29
21:20 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk. Launch Vehicle: Ute Tomahawk.1976 June 29
Launch Site: Baikonur. Launch Complex: Baikonur LC177. Launch Vehicle: MR-UR-100.1976 June 29
Launch Site: Baikonur. Launch Complex: Baikonur LC103. LV Family: R-36M. Launch Vehicle: R-36M 15A14.1976 June 29
07:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.- Cosmos 835 - . Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: Vostok. Spacecraft: Zenit-4MK. Duration: 13.00 days. Decay Date: 1976-07-12 . USAF Sat Cat: 8922 . COSPAR: 1976-060A. Apogee: 317 km (196 mi). Perigee: 174 km (108 mi). Inclination: 65.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 June 29
08:12 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.- Cosmos 836 - . Mass: 750 kg (1,650 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft Bus: KAUR-1. Spacecraft: Strela-2M. USAF Sat Cat: 8923 . COSPAR: 1976-061A. Apogee: 801 km (497 mi). Perigee: 773 km (480 mi). Inclination: 74.10 deg. Period: 100.60 min.
1976 June 29
18:20 GMT - . Launch Site: White Sands. LV Family: Tomahawk. Launch Vehicle: Nike Tomahawk.1976 June 29
18:20 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170.1977 June 29
18:34 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92M.- Meteor 1-28 - . Payload: Meteor-Priroda s/n 2-2. Mass: 3,800 kg (8,300 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Weather satellite. Spacecraft Bus: Meteor. Spacecraft: Meteor-Priroda. Decay Date: 1993-08-28 . USAF Sat Cat: 10113 . COSPAR: 1977-057A. Apogee: 338 km (210 mi). Perigee: 332 km (206 mi). Inclination: 97.40 deg. Period: 91.20 min. Continuation of experimental work in studying the natural resources of the earth. Acquisition of meteorological information required for use in the operational weather service. .
1978 June 29
Launch Site: Baikonur. Launch Complex: Baikonur LC102. LV Family: R-36M. Launch Vehicle: R-36M 15A14.1978 June 29
22:24 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.- Comstar 3 - .
Payload: Comstar 1C. Mass: 1,520 kg (3,350 lb). Nation: USA.
Agency: Comsat.
Program: Comstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: HS 312 / HS 351 / HS 353.
Spacecraft: Intelsat 4A.
Completed Operations Date: 1986-05-21 . USAF Sat Cat: 10975 . COSPAR: 1978-068A. Apogee: 36,172 km (22,476 mi). Perigee: 36,007 km (22,373 mi). Inclination: 11.50 deg. Period: 1,451.60 min.
US domestic telephone service. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit over the Americas at 87 deg W in 1978-1984 over the Americas at 76 deg W in 1984-1986 As of 1 September 2001 located at 101.79 deg W drifting at 3.884 deg W per day. As of 2007 Mar 4 located at 39.19E drifting at 3.878W degrees per day.
1979 June 29
Launch Site: Baikonur. Launch Complex: Baikonur LC170. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100U 15A16.1979 June 29
Launch Site: Thumba. LV Family: RH. Launch Vehicle: RH-200.1979 June 29
08:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant VB.1979 June 29
16:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-U.- Cosmos 1111 - . Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: Vostok. Spacecraft: Zenit-6U. Duration: 15.00 days. Decay Date: 1979-07-14 . USAF Sat Cat: 11429 . COSPAR: 1979-061A. Apogee: 354 km (219 mi). Perigee: 255 km (158 mi). Inclination: 62.80 deg. Period: 90.60 min. Photo surveillance; returned film capsule..
1980 June 29
04:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.- Progress 10 - .
Payload: Progress s/n 110. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 35.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 19.88 days. Completed Operations Date: 1980-07-19 01:47:18 . Decay Date: 1980-07-19 01:47:18 . USAF Sat Cat: 11867 . COSPAR: 1980-055A. Apogee: 264 km (164 mi). Perigee: 183 km (113 mi). Inclination: 51.60 deg. Period: 89.00 min.
Unmanned supply vessel for Salyut 6. Delivery of various cargoes to the Salyut-6 orbital station. Docked with Salyut 6 on 1 Jul 1980 05:53:00 GMT. Undocked on 17 Jul 1980 22:21:00 GMT. Destroyed in reentry on 19 Jul 1980 01:47:00 GMT. Total free-flight time 3.19 days. Total docked time 16.69 days.
1981 June 29
13:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC43. LV Family: Deacon. Launch Vehicle: Rocketsonde.1982 June 29
- STS-4 - Wakeup Song: Hold That Tiger - . Flight: STS-4. "Hold That Tiger" by Auburn University Band.
1982 June 29
11:01 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Taurus Orion.1982 June 29
21:45 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.- Cosmos 1383 - . Payload: Nadezhda 11F643N s/n 514. Mass: 810 kg (1,780 lb). Nation: Russia. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Nadezhda. USAF Sat Cat: 13301 . COSPAR: 1982-066A. Apogee: 1,025 km (636 mi). Perigee: 986 km (612 mi). Inclination: 82.90 deg. Period: 105.20 min. Trials of experimental equipment for testing systems to determine the location of vessels and aircraft in distress..
1983 June 29
04:35 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 8C.1984 June 29
Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral ETR. Launch Platform: SSBN 625. LV Family: Polaris. Launch Vehicle: Poseidon C3.1984 June 29
00:21 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.- Cosmos 1579 - . Mass: 3,800 kg (8,300 lb). Nation: Russia. Agency: MO. Program: RORSAT. Class: Surveillance. Type: Naval Radarsat. Spacecraft Bus: Kosmoplan. Spacecraft: US-A. Decay Date: 1984-11-05 . USAF Sat Cat: 15328 . COSPAR: 1984-069C. Apogee: 970 km (600 mi). Perigee: 914 km (567 mi). Inclination: 65.10 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1984 June 29
15:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-U.- Cosmos 1580 - . Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: Vostok. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1984-07-13 . USAF Sat Cat: 15090 . COSPAR: 1984-070A. Apogee: 345 km (214 mi). Perigee: 241 km (149 mi). Inclination: 62.80 deg. Period: 90.40 min. Military cartographic satellite; returned film capsule..
1984 June 29
20:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral ETR. Launch Platform: SSBN 625. LV Family: Polaris. Launch Vehicle: Poseidon C3.1987 June 29
11:06 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A.1988 June 29
Launch Site: Balasore. LV Family: RH. Launch Vehicle: RH-200.1991 June 29
14:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G-1.- REX - . Payload: REX 1. Mass: 85 kg (187 lb). Nation: USA. Agency: USAF Rome. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: GemStar. Spacecraft: REX. USAF Sat Cat: 21527 . COSPAR: 1991-045A. Apogee: 869 km (539 mi). Perigee: 767 km (476 mi). Inclination: 89.50 deg. Period: 101.30 min. Radiation Experiment; tested communications components in high radiation environment. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..
1992 June 29
21:15 GMT - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Rocketsonde.1994 June 29
02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P.1995 June 29
- STS-71 - Wakeup Song: From a Distance - . Flight: STS-71. "From a Distance" by Nancy Griffith. It was preceded by special birthday greetings to Pilot Charlie Precourt from his wife and daughters..
1995 June 29
Launch Site: Barking Sands. LV Family: Strypi. Launch Vehicle: Strypi IX.- ETCE-12 Target mission - . Nation: USA. Agency: USA SMDC. Type: ABM Target. Apogee: 200 km (120 mi).
1996 June 29
- STS-78 - Wakeup Song: Another Saturday Night - . Flight: STS-78. "Another Saturday Night" by Max Q, the all-astronaut band, with Susan Helms on keyboards CAPCOM: Bill McArthur.
1997 June 29
- Death of Josef Martin Michel - . Nation: Germany, USA. Related Persons: Michel, Josef. German engineer in WW2, member of the Rocket Team in the United States thereafter..
2000 June 29
- ISS Status Report: ISS 00-25 - .
Nation: USA.
Program: ISS.
After a week of comprehensive reviews by program managers on both sides of the Atlantic Ocean, the next component of the International Space Station (ISS) is poised for launch to provide the early living quarters for the first permanent occupants of the orbital outpost. Additional Details: here....
2000 June 29
- Death of Hermann H Kurzweg - . Nation: Germany, USA. Related Persons: Kurzweg. German-American aerodynamicist, at Peenemuende, then US Naval Ordnance 1946-1960, NASA 1960-1974..
2001 June 29
00:44 GMT - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant VC.2002 June 29
- International Space Station Status Report #02-29 - .
Nation: USA.
Related Persons: Korzun,
Whitson.
Program: ISS.
Flight: STS-111 ISS EO-5.
A Russian Progress resupply craft docked to the International Space Station early today, three days after its launch from the Baikonur Cosmodrome in Kazakhstan. Aboard the unpiloted Progress 8 are food, fuel and supplies for the space station and its Expedition 5 crew. Additional Details: here....
2004 June 29
03:58 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: Odyssey. LV Family: Zenit. Launch Vehicle: Zenit-3SL. FAILURE: Partial failure - upper stage left satellite stranded in useless orbit.. Failed Stage: 3.- Apstar 5 - . Payload: Apstar 1R, Telstar 18, LS-1300. Mass: 4,640 kg (10,220 lb). Nation: China. Agency: APT Satellite Company. Manufacturer: Palo Alto. Program: Apstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28364 . COSPAR: 2004-024A. Apogee: 35,799 km (22,244 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Delayed from November 2003, April 28 2004. Partial failure (upper stage). As of 2007 Mar 11 located at 138.01E drifting at 0.009W degrees per day..
2004 June 29
06:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.- Aprizesat 2 (LatinSat D) - . Mass: 12 kg (26 lb). Nation: Argentina. Agency: Aprize. Program: AIS. Class: Communications. Type: Civilian store-dump communications satellite. Spacecraft: AprizeSat. USAF Sat Cat: 28366 . COSPAR: 2004-025A. Apogee: 853 km (530 mi). Perigee: 695 km (431 mi). Inclination: 98.30 deg. Period: 100.30 min. Delayed from March. 31.
- Demeter - .
Mass: 125 kg (275 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Seismology satellite. Spacecraft Bus: Myriade.
Spacecraft: Demeter.
USAF Sat Cat: 28368 . COSPAR: 2004-025C. Apogee: 723 km (449 mi). Perigee: 695 km (431 mi). Inclination: 98.30 deg. Period: 99.00 min.
Demeter studied disturbances of the ionosphere due to seismo electromagnetic effects and human activities (power lines, VLF transmitters, HF broadcasting stations). Study of natural electromagnetic emissions in the ULF/ELF/VLF range related to seismic or volcanic activity could be used to predict earthquatkes or eruptions in advance. Demeter tracked these emissions and other space plasma parameters (ion composition, electron density and temperature, energetic particles). The scientific payload consisted of three electric and three magnetic sensors (covering six components of the electromagnetic field from DC to 3.5 MHz); a Langmuir probe; an ion spectrometer; and an energetic particle analyzer. 8 Gbits of onboard memory recorded the data, which was returned to earth as 18 Mb/s high bit rate telemetry in the X band. The two-year mission was handled from a control center in Toulouse.
- Saudicomsat 1 - . Mass: 12 kg (26 lb). Nation: Saudi Arabia. Agency: RSRI. Manufacturer: KACST. Class: Communications. Type: Civilian communications satellite. Spacecraft: SaudiSat. USAF Sat Cat: 28369 . COSPAR: 2004-025D. Apogee: 751 km (466 mi). Perigee: 699 km (434 mi). Inclination: 98.30 deg. Period: 99.30 min. Amateur store-forward communications payload..
- Saudicomsat 2 - . Mass: 12 kg (26 lb). Nation: Saudi Arabia. Agency: RSRI. Manufacturer: KACST. Class: Communications. Type: Civilian communications satellite. Spacecraft: SaudiSat. USAF Sat Cat: 28370 . COSPAR: 2004-025E. Apogee: 783 km (486 mi). Perigee: 698 km (433 mi). Inclination: 98.30 deg. Period: 99.60 min. Amateur store-forward communications payload..
- Saudisat 2 - . Mass: 35 kg (77 lb). Nation: Saudi Arabia. Agency: RSRI. Manufacturer: KACST. Class: Technology. Type: Navigation technology satellite. Spacecraft: SaudiSat. USAF Sat Cat: 28371 . COSPAR: 2004-025F. Apogee: 736 km (457 mi). Perigee: 698 km (433 mi). Inclination: 98.30 deg. Period: 99.10 min. Experimental technology satellite that included imaging with resolution better than 15 m for remote sensing..
- Aprizesat 1 (LatinSat C) - . Mass: 12 kg (26 lb). Nation: Argentina. Agency: Makeyev bureau. Program: AIS. Class: Communications. Type: Civilian store-dump communications satellite. Spacecraft: AprizeSat. USAF Sat Cat: 28372 . COSPAR: 2004-025G. Apogee: 767 km (476 mi). Perigee: 698 km (433 mi). Inclination: 98.30 deg. Period: 99.50 min.
- Unisat 3 - . Mass: 12 kg (26 lb). Nation: Italy. Agency: La Sapienza. Class: Technology. Type: Navigation technology satellite. Spacecraft: UniSat. USAF Sat Cat: 28373 . COSPAR: 2004-025H. Apogee: 800 km (490 mi). Perigee: 684 km (425 mi). Inclination: 98.30 deg. Period: 99.80 min.
- Amsat Echo - . Mass: 12 kg (26 lb). Nation: USA. Agency: AmSat. Program: Oscar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Amsat Echo. USAF Sat Cat: 28375 . COSPAR: 2004-025K. Apogee: 818 km (508 mi). Perigee: 697 km (433 mi). Inclination: 98.30 deg. Period: 100.00 min.
2004 June 29
07:25 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Shtil'.2007 June 29
10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2M.- Cosmos 2428 - . Mass: 3,200 kg (7,000 lb). Nation: Russia. Agency: VKS. Manufacturer: Yuzhnoye. Class: Surveillance. Type: SIGINT. Spacecraft: Tselina-2. USAF Sat Cat: 31792 . COSPAR: 2007-029A. Apogee: 857 km (532 mi). Perigee: 846 km (525 mi). Inclination: 71.00 deg. Period: 102.00 min. Signals intelligence satellite. First launch in three years, and first with the improved version of the Zenit-2 launch vehicle using components developed for the Zenit-3SL..
2008 June 29
- ISS On-Orbit Status 06/29/08 - . Nation: USA. Related Persons: Kononenko, Love, Volkov, Sergey. Program: ISS. Flight: Soyuz TMA-12. Sunday -- off-duty for CDR Volkov, FE-1 Kononenko and FE-2 Chamitoff.. Additional Details: here....
2009 June 29
07:30 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant IX.- NASA 36.244UG - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi). UV Astron.
2009 June 29
10:01 GMT - . Launch Site: Vandenberg. LV Family: Minuteman. Launch Vehicle: Minuteman 3.2010 June 29
07:32 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands MLP. Launch Platform: MLP. LV Family: R-11. Launch Vehicle: Scud.2010 June 29
07:37 GMT - . Launch Site: Barking Sands. Launch Vehicle: THAAD.2012 June 29
Launch Site: Mojave. Launch Complex: Mojave RW12/30. Launch Platform: WK2. LV Family: Spaceship. Launch Vehicle: Spaceship Two.2012 June 29
13:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC37B. Launch Pad: SLC37B. LV Family: Delta IV. Launch Vehicle: Delta 4H.- USA 237 - . Payload: Orion 8 / NROL-15. Mass: 5,400 kg (11,900 lb). Nation: USA. Class: Surveillance. Type: SIGINT. Spacecraft: Advanced Orion. USAF Sat Cat: 38528 . COSPAR: 2012-034A. Apogee: 35,800 km (22,200 mi). Perigee: 35,800 km (22,200 mi). Inclination: 0.00 deg. Period: 1,440.00 min. Probable geosynchronous signals intelligence satellite..
2014 June 29
Launch Site: Gitdaeryung. LV Family: R-11. Launch Vehicle: Hwasong 6.- Nation: Korea North. Agency: KP. Apogee: 150 km (90 mi).
2014 June 29
Launch Site: Gitdaeryung. LV Family: R-11. Launch Vehicle: Hwasong 6.- Nation: Korea North. Agency: KP. Apogee: 150 km (90 mi).
2016 June 29
03:21 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: Chang Zheng 4B.- Shi Jian 16-02 - . Payload: SJ 16-02. Nation: China. Class: Surveillance. Type: ELINT. Spacecraft: DFH-4. USAF Sat Cat: 41634 . COSPAR: 2016-043A. Apogee: 616 km (382 mi). Perigee: 596 km (370 mi). Inclination: 75.00 deg. Chinese technology satellite..
2017 June 29
08:25 GMT - . Launch Site: Wallops Island. LV Family: Malemute. Launch Vehicle: Terrier Improved Malemute.- NASA 46.015GT - . Nation: USA. Apogee: 189 km (117 mi). Test/Aeronomy mission. Impacted Atlantic..
2018 June 29
09:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.- Dragon CRS-15 - . Payload: Dragon C111. Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 43522 . COSPAR: 2018-055A. Apogee: 409 km (254 mi). Perigee: 402 km (249 mi). Inclination: 51.64 deg. Period: 92.68 min. See Dragon CRS-15 (SpX 15, Dragon C111-F2). ..
- UiTMSAT-1 - . Payload: Univ. Tek. MARA-Sat-1. Nation: Malaysia. COSPAR: 2018-055. See Bird MYS (UiTMSAT 1) ↑. 1U cubesat by Universiti Teknologi MARA. Mission: Technology demonstration. Status as of 2019: Active. ..
- Biarri-Squad 1 - . COSPAR: 2018-055. See Biarri-Squad 1 ↑. ..
- Maya-1 - . Nation: Japan. COSPAR: 2018-055. See Bird PHL (MAYA 1) ↑. 1U cubesat by Kyushu Institute of Technology. Mission: Technology demonstration. Status as of 2019: Active. ..
- Bhutan-1 - . Nation: Japan. COSPAR: 2018-055. See Bird BTN (Bhutan 1) ↑. 1U cubesat by Kyushu Institute of Technology. Mission: Technology demonstration. Status as of 2019: Active..
- Biarri-Squad 3 - . COSPAR: 2018-055. See Biarri-Squad 3 ↑. ..
- Biarri-Squad 2 - . COSPAR: 2018-055. See Biarri-Squad 2 ↑. ..