Kosmos 265: Difference between revisions
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| spacecraft_type = [[DS-P1-Yu]] |
| spacecraft_type = [[DS-P1-Yu]] |
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| manufacturer = [[Yuzhnoye Design Bureau|Yuzhnoye]] |
| manufacturer = [[Yuzhnoye Design Bureau|Yuzhnoye]] |
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| launch_mass = {{convert|325|kg}} |
| launch_mass = {{convert|325|kg|lb|abbr=on}} |
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| launch_date = {{start-date|7 February 1969, 13:59|timezone=yes}} UTC |
| launch_date = {{start-date|7 February 1969, 13:59|timezone=yes}} UTC |
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| orbit_reference = [[Geocentric orbit|Geocentric]] |
| orbit_reference = [[Geocentric orbit|Geocentric]] |
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| orbit_regime = [[Low Earth orbit|Low Earth]] |
| orbit_regime = [[Low Earth orbit|Low Earth]] |
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| orbit_periapsis = {{convert|261|km}} |
| orbit_periapsis = {{convert|261|km|mi|abbr=on}} |
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| orbit_apoapsis = {{convert|413|km}} |
| orbit_apoapsis = {{convert|413|km|mi|abbr=on}} |
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| orbit_inclination = 70.9 degrees |
| orbit_inclination = 70.9 degrees |
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| orbit_period = 91.3 minutes |
| orbit_period = 91.3 minutes |
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| apsis = gee |
| apsis = gee |
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}} |
}} |
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'''Kosmos 265''' ({{lang-ru|Космос 265}} meaning ''Cosmos 265''), known before launch as '''DS-P1-Yu No.21''', was a [[Soviet Union|Soviet]] [[satellite]] which was used as a radar calibration target for tests of [[anti-ballistic missile]]s. It was built by the [[Yuzhnoye Design Bureau]], and launched in 1969 as part of the |
'''Kosmos 265''' ({{lang-ru|Космос 265}} meaning ''Cosmos 265''), known before launch as '''DS-P1-Yu No.21''', was a [[Soviet Union|Soviet]] [[satellite]] which was used as a radar calibration target for tests of [[anti-ballistic missile]]s. It was built by the [[Yuzhnoye Design Bureau]], and launched in 1969 as part of the Dnepropetrovsk Sputnik programme.<ref name="EA-DSP1Yu">{{cite web |url=http://www.astronautix.com/craft/dsp1yu.htm |title=DS-P1-Yu |last=Wade |first=Mark |publisher=Encyclopedia Astronautica |accessdate=13 August 2009}}</ref> It had a mass of {{convert|325|kg|lb|abbr=on}}.<ref name="EA-DSP1Yu"/> |
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Kosmos 265 was launched from |
Kosmos 265 was launched from Plesetsk Cosmodrome Site 133/1,<ref name="JSR-LL">{{cite web |url=http://planet4589.org/space/log/launchlog.txt |title=Launch Log |last=McDowell |first=Jonathan |publisher=Jonathan's Space Page |accessdate=13 August 2009}}</ref> atop a Kosmos-2I 63SM [[carrier rocket]]. The launch occurred on 7 February 1969 at 13:59 UTC, and resulted in Kosmos 265's successful deployment into low Earth orbit.<ref name="EA-K2">{{cite web |url=http://www.astronautix.com/lvs/kosmos2.htm |title=Kosmos 2 |last=Wade |first=Mark |publisher=Encyclopedia Astronautica |accessdate=13 August 2009}}</ref> Upon reaching orbit, it was assigned its [[Cosmos (satellite)|Kosmos]] designation, and received the [[International Designator]] 1969-012A. |
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Kosmos 265 was operated in an orbit with a [[apsis|perigee]] of {{convert|261|km}}, an [[apsis|apogee]] of {{convert|413|km}}, 70.9 degrees of [[inclination]], and an [[orbital period]] of 91.3 minutes.<ref name="EA-DSP1Yu"/><ref name="JSR-SC"/> It remained in orbit until it [[orbital decay|decayed]] and reentered the atmosphere on 1 May 1969.<ref name="JSR-SC">{{cite web|url=http://www.planet4589.org/space/log/satcat.txt|title=Satellite Catalog|last=McDowell|first=Jonathan|publisher=Jonathan's Space Page|accessdate=13 August 2009}}</ref> It was the eighteenth of seventy nine |
Kosmos 265 was operated in an orbit with a [[apsis|perigee]] of {{convert|261|km|mi|abbr=on}}, an [[apsis|apogee]] of {{convert|413|km|mi|abbr=on}}, 70.9 degrees of [[inclination]], and an [[orbital period]] of 91.3 minutes.<ref name="EA-DSP1Yu"/><ref name="JSR-SC"/> It remained in orbit until it [[orbital decay|decayed]] and reentered the atmosphere on 1 May 1969.<ref name="JSR-SC">{{cite web |url=http://www.planet4589.org/space/log/satcat.txt |title=Satellite Catalog |last=McDowell |first=Jonathan |publisher=Jonathan's Space Page |accessdate=13 August 2009}}</ref> It was the eighteenth of seventy nine DS-P1-Yu satellites to be launched,<ref name="EA-DSP1Yu"/> and the seventeenth of seventy two to successfully reach orbit.<ref name="GSP">{{cite web |url=http://space.skyrocket.de/doc_sdat/ds-p1-yu.htm |title=DS-P1-Yu (11F618) |first=Gunter |last=Krebs |publisher=Gunter's Space Page |accessdate=13 August 2009}}</ref> |
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== See also == |
== See also == |
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{{Portal|Spaceflight}} |
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* [[1969 in spaceflight]] |
* [[1969 in spaceflight]] |
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{{-}} |
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== References == |
== References == |
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{{Dnepropetrovsk Sputnik}} |
{{Dnepropetrovsk Sputnik}} |
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{{Orbital launches in 1969}} |
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[[Category:Spacecraft launched in 1969]] |
[[Category:Spacecraft launched in 1969]] |
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[[Category:Kosmos satellites]] |
[[Category:Kosmos satellites]] |
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{{USSR-spacecraft-stub}} |
{{USSR-spacecraft-stub}} |
Revision as of 22:31, 24 January 2014
Mission type | ABM radar target |
---|---|
COSPAR ID | 1969-012A |
SATCAT no. | 03675 |
Spacecraft properties | |
Spacecraft type | DS-P1-Yu |
Manufacturer | Yuzhnoye |
Launch mass | 325 kg (717 lb) |
Start of mission | |
Launch date | 7 February 1969, 13:59 | UTC
Rocket | Kosmos-2I 63SM |
Launch site | Plesetsk 133/1 |
End of mission | |
Decay date | 1 May 1969 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 261 km (162 mi) |
Apogee altitude | 413 km (257 mi) |
Inclination | 70.9 degrees |
Period | 91.3 minutes |
Kosmos 265 (Russian: Космос 265 meaning Cosmos 265), known before launch as DS-P1-Yu No.21, was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was built by the Yuzhnoye Design Bureau, and launched in 1969 as part of the Dnepropetrovsk Sputnik programme.[1] It had a mass of 325 kg (717 lb).[1]
Kosmos 265 was launched from Plesetsk Cosmodrome Site 133/1,[2] atop a Kosmos-2I 63SM carrier rocket. The launch occurred on 7 February 1969 at 13:59 UTC, and resulted in Kosmos 265's successful deployment into low Earth orbit.[3] Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1969-012A.
Kosmos 265 was operated in an orbit with a perigee of 261 km (162 mi), an apogee of 413 km (257 mi), 70.9 degrees of inclination, and an orbital period of 91.3 minutes.[1][4] It remained in orbit until it decayed and reentered the atmosphere on 1 May 1969.[4] It was the eighteenth of seventy nine DS-P1-Yu satellites to be launched,[1] and the seventeenth of seventy two to successfully reach orbit.[5]
See also
References
- ^ a b c d Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Retrieved 13 August 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 13 August 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 13 August 2009.
- ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 13 August 2009.
- ^ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 13 August 2009.