From Wikipedia, the free encyclopedia
Kosmos 219
(
Russian
:
Космос 219
meaning
Cosmos 219
), also known as
DS-U2-D No.2
, was a
Soviet
satellite
which was launched in 1968 as part of the
Dnepropetrovsk Sputnik
programme. It was a 400 kilograms (880 lb) spacecraft,
[1]
which was built by the
Yuzhnoye Design Bureau
, and was used to investigate flows of
charged particles
in the
magnetosphere
of the Earth.
[1]
A
Kosmos-2I
63SM
carrier rocket
was used to launch Kosmos 219 into
low Earth orbit
. The launch took place from
Site 86/4
at
Kapustin Yar
.
[2]
The launch occurred at 04:42:56 GMT on 26 April 1968, and resulted in the successful insertion of the satellite into orbit.
[3]
Upon reaching orbit, the satellite was assigned its
Kosmos
designation, and received the
International Designator
1968-038A.
[4]
The
North American Aerospace Air Command
assigned it the
catalogue number
03220.
Kosmos 219 was the second of two
DS-U2-D
satellites to be launched,
[1]
after
Kosmos 137
.
[5]
It was operated in an orbit with a
perigee
of 215 kilometres (134 mi), an
apogee
of 1,745 kilometres (1,084 mi), 48.4° of
inclination
, and an
orbital period
of 104.7 minutes.
[6]
It completed operations on 28 February 1969,
[7]
before
decaying
from orbit and
reentering
the atmosphere on 2 March.
[6]
See also
[
edit
]
References
[
edit
]
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DS-1
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DS-2
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DS-A1
| |
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DS-K
| |
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DS-MG
| |
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DS-MT
| |
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DS-MO
| |
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DS-P1
| |
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DS-U1
| |
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DS-U2
| |
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DS-U3
| |
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Omega
| |
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|
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|
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in
underline
. Uncatalogued launch failures are listed in
italics
. Payloads deployed from other spacecraft are denoted in (brackets).
|