Kosmos 388
In today's world, Kosmos 388 has become a topic of great relevance and interest to a wide variety of people. Whether because of its impact on society, its historical relevance, or its influence on popular culture, Kosmos 388 has sparked curiosity and debate among experts and fans alike. Over the years, Kosmos 388 has demonstrated its ability to generate discussion and reflection in different contexts and disciplines, becoming a key point in the understanding and analysis of various aspects of modern life. In this article, we will explore different facets of Kosmos 388 and its impact today, with the aim of understanding its importance and the implications it has for our society.
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1970-112A |
| SATCAT no. | 04811 |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 325 kilograms (717 lb) |
| Start of mission | |
| Launch date | 18 December 1970, 09:39:13 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 10 May 1971 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 263 kilometres (163 mi) |
| Apogee altitude | 479 kilometres (298 mi) |
| Inclination | 70.9 degrees |
| Period | 92 minutes |
Kosmos 388 (Russian: Космос 388 meaning Cosmos 388), known before launch as DS-P1-Yu No.43, was a Soviet satellite which was launched in 1970 as part of the Dnepropetrovsk Sputnik programme. It was a 325-kilogram (717 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests.[1]
Launch
Kosmos 388 was successfully launched into low Earth orbit on 18 December 1970, with the rocket lifting off at 09:39:13 UTC.[2] The launch took place from Site 133/1 at the Plesetsk Cosmodrome,[3] and used a Kosmos-2I 63SM carrier rocket. Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1970-112A.[4]
Orbit
Kosmos 388 was the thirty-eighth of seventy nine DS-P1-Yu satellites to be launched,[1] and the thirty-fifth of seventy two to successfully reach orbit.[5] It was operated in an orbit with a perigee of 263 kilometres (163 mi), an apogee of 479 kilometres (298 mi), 70.9 degrees of inclination, and an orbital period of 92 minutes.[1][6] It remained in orbit until it decayed and reentered the atmosphere on 10 May 1971.[6]
References
- ^ a b c Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 15 August 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 15 August 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 15 August 2009.
- ^ "Cosmos 388". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 15 August 2009.
- ^ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 15 August 2009.
- ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 15 August 2009.
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