| Mission type | Technology |
|---|---|
| COSPAR ID | 1965-084A |
| SATCAT no. | 01629 |
| Mission duration | 76 days |
| Spacecraft properties | |
| Spacecraft type | DS-U2-V |
| Manufacturer | Yuzhnoye |
| Launch mass | 305 kg [1] |
| Start of mission | |
| Launch date | 19 October 1965, 05:45:00 GMT |
| Rocket | Kosmos-2M 63S1M |
| Launch site | Kapustin Yar, Site 86/1 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 3 January 1966 |
| Orbital parameters | |
| Reference system | Geocentric [2] |
| Regime | Low Earth |
| Perigee altitude | 216 km |
| Apogee altitude | 513 km |
| Inclination | 48.4° |
| Period | 91.7 minutes |
| Epoch | 19 October 1965 |
Kosmos 93 ( Russian: Космос 93 meaning Cosmos 93), also known as DS-U2-V No.1, was a Soviet satellite which was launched in 1965 as part of the Dnepropetrovsk Sputnik programme. It was a 305 kilograms (672 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to conduct classified technology development experiments for the Soviet armed forces. [3]
A Kosmos-2M 63S1M [4] carrier rocket was used to launch Kosmos 93 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar. [5] The launch occurred at 05:45 GMT on 19 October 1965, and resulted in the successful insertion of the satellite into orbit. [6] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1965-084A. [7] The North American Air Defense Command assigned it the catalogue number 01629.
Kosmos 93 was the first of four DS-U2-V satellites to be launched. [8] It was operated in an orbit with a perigee of 216 kilometres (134 mi), an apogee of 513 kilometres (319 mi), an 48.4° of inclination, and an orbital period of 91.7 minutes. On 3 January 1966, it decayed from orbit and reentered the atmosphere. [9] [10]
See also
References
- ^ "Cosmos 93". NASA. 27 February 2020. Retrieved 25 November 2022.
- ^ "Cosmos 98 Trajectory". NASA. 27 February 2020. Retrieved 25 November 2022.
- ^ Wade, Mark. "DS-U2-V". Encyclopedia Astronautica. Archived from the original on 5 January 2009. Retrieved 6 December 2009.
- ^ Wade, Mark (31 October 2001). "Kosmos 63S1M". Encyclopedia Astronautica. Archived from the original on 25 July 2012. Retrieved 14 January 2010.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 6 December 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 6 December 2009.
- ^ "Cosmos 93". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 6 December 2009.
- ^ Krebs, Gunter. "DS-U2-V". Gunter's Space Page. Retrieved 25 November 2022.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 6 December 2009.
- ^ "World Civil Satellites 1957-2006". Space Security Index. Archived from the original on 18 July 2011. Retrieved 6 December 2009.
 | This article about one or more spacecraft of the Soviet Union is a stub. You can help Wikipedia by expanding it. |
| Mission type | Technology |
|---|---|
| COSPAR ID | 1965-084A |
| SATCAT no. | 01629 |
| Mission duration | 76 days |
| Spacecraft properties | |
| Spacecraft type | DS-U2-V |
| Manufacturer | Yuzhnoye |
| Launch mass | 305 kg [1] |
| Start of mission | |
| Launch date | 19 October 1965, 05:45:00 GMT |
| Rocket | Kosmos-2M 63S1M |
| Launch site | Kapustin Yar, Site 86/1 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 3 January 1966 |
| Orbital parameters | |
| Reference system | Geocentric [2] |
| Regime | Low Earth |
| Perigee altitude | 216 km |
| Apogee altitude | 513 km |
| Inclination | 48.4° |
| Period | 91.7 minutes |
| Epoch | 19 October 1965 |
Kosmos 93 ( Russian: Космос 93 meaning Cosmos 93), also known as DS-U2-V No.1, was a Soviet satellite which was launched in 1965 as part of the Dnepropetrovsk Sputnik programme. It was a 305 kilograms (672 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to conduct classified technology development experiments for the Soviet armed forces. [3]
A Kosmos-2M 63S1M [4] carrier rocket was used to launch Kosmos 93 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar. [5] The launch occurred at 05:45 GMT on 19 October 1965, and resulted in the successful insertion of the satellite into orbit. [6] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1965-084A. [7] The North American Air Defense Command assigned it the catalogue number 01629.
Kosmos 93 was the first of four DS-U2-V satellites to be launched. [8] It was operated in an orbit with a perigee of 216 kilometres (134 mi), an apogee of 513 kilometres (319 mi), an 48.4° of inclination, and an orbital period of 91.7 minutes. On 3 January 1966, it decayed from orbit and reentered the atmosphere. [9] [10]
See also
References
- ^ "Cosmos 93". NASA. 27 February 2020. Retrieved 25 November 2022.
- ^ "Cosmos 98 Trajectory". NASA. 27 February 2020. Retrieved 25 November 2022.
- ^ Wade, Mark. "DS-U2-V". Encyclopedia Astronautica. Archived from the original on 5 January 2009. Retrieved 6 December 2009.
- ^ Wade, Mark (31 October 2001). "Kosmos 63S1M". Encyclopedia Astronautica. Archived from the original on 25 July 2012. Retrieved 14 January 2010.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 6 December 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 6 December 2009.
- ^ "Cosmos 93". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 6 December 2009.
- ^ Krebs, Gunter. "DS-U2-V". Gunter's Space Page. Retrieved 25 November 2022.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 6 December 2009.
- ^ "World Civil Satellites 1957-2006". Space Security Index. Archived from the original on 18 July 2011. Retrieved 6 December 2009.
| This article about one or more spacecraft of the Soviet Union is a stub. You can help Wikipedia by expanding it. |