From Wikipedia, the free encyclopedia
Soviet satellite
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 kilometres (162 mi), an
apogee
of 413 kilometres (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
[
edit
]
References
[
edit
]
- ^
a
b
c
d
Wade, Mark.
"DS-P1-Yu"
. Encyclopedia Astronautica. Archived from
the original
on 2 June 2012
. Retrieved
13 August
2009
.
- ^
McDowell, Jonathan.
"Launch Log"
. Jonathan's Space Page
. Retrieved
13 August
2009
.
- ^
Wade, Mark.
"Kosmos 2"
. Encyclopedia Astronautica. Archived from
the original
on 18 June 2012
. 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
.
|
---|
DS-1
| |
---|
DS-2
| |
---|
DS-A1
| |
---|
DS-K
| |
---|
DS-MG
| |
---|
DS-MT
| |
---|
DS-MO
| |
---|
DS-P1
| |
---|
DS-U1
| |
---|
DS-U2
| |
---|
DS-U3
| |
---|
Omega
| |
---|
|
---|
|
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).
|