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・ Kosmos 2209
・ Kosmos 221
・ Kosmos 2217
・ Kosmos 222
・ Kosmos 2221
・ Kosmos 2222
・ Kosmos 2224
・ Kosmos 2229
・ Kosmos 2232
・ Kosmos 2241
・ Kosmos 225
・ Kosmos 2251
・ Kosmos 2261
・ Kosmos 2282
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Kosmos 23
・ Kosmos 230
・ Kosmos 2312
・ Kosmos 233
・ Kosmos 2340
・ Kosmos 2342
・ Kosmos 2345
・ Kosmos 2350
・ Kosmos 2351
・ Kosmos 2368
・ Kosmos 2379
・ Kosmos 238
・ Kosmos 2380
・ Kosmos 2381
・ Kosmos 2382


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Kosmos 23 : ウィキペディア英語版
Kosmos 23

Kosmos 23 ((ロシア語:Космос 23) meaning ''Cosmos 23''), also known as Omega No.2, was a satellite which was launched by the Soviet Union in 1963. It was an Omega satellite, derived from the Dnepropetrovsk Sputnik series. It was a spacecraft,〔 which was built by the Yuzhnoye Design Bureau, and was used to conduct experiments with the use of gyroscopes to control spacecraft, for VNIIEM.
Kosmos 23 was launched from pad 2 of the Mayak Launch Complex at Kapustin Yar, aboard a Kosmos-2I 63S1 carrier rocket. The launch occurred at 14:15:00 UTC on 13 December 1963, and resulted in the successful insertion of the satellite into a low Earth orbit. Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1963-050A. The North American Aerospace Defense Command assigned it the catalogue number 00707.
Kosmos 23 was the second of two Omega satellites to be launched,〔 after Kosmos 14. It was operated in an orbit with a perigee of , an apogee of , 48.9 degrees of inclination, and an orbital period of 92.2 minutes.〔 It remained in orbit until it decayed and reentered the atmosphere on 27 March 1964.
==See also==

*1963 in spaceflight

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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