To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.

From Wikipedia, the free encyclopedia

Kosmos 136
Mission typeOptical imaging reconnaissance
COSPAR ID1966-115A
SATCAT no.02624
Mission duration8 days
Spacecraft properties
Spacecraft typeZenit-2
Launch mass4730 kg [1]
Start of mission
Launch date19 December 1966
12:00:01 GMT
RocketVostok-2 s/n N15001-09
Launch sitePlesetsk, Site 41/1
End of mission
Landing date27 December 1966
06:00 GMT [2]
Orbital parameters
Reference systemGeocentric [3]
RegimeLow Earth
Perigee altitude188 km
Apogee altitude280 km
Period89.4 minutes
Epoch19 December 1966

Kosmos 136 (Russian: Космос 136 meaning Cosmos 136) or Zenit-2 No.47 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 136 was the forty-fourth of eighty-one such satellites to be launched[4][5] and had a mass of 4,730 kilograms (10,430 lb). In addition to its reconnaissance mission, the satellite was also used for scientific research.

Kosmos 136 was launched by a Vostok-2 rocket, serial number N15001-09,[6] flying from Site 41/1 at the Plesetsk Cosmodrome. The launch took place at 12:00:01 GMT on 19 December 1966,[7] and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1966-115A and the Satellite Catalog Number 02624.[1]

Kosmos 136 was operated in a low Earth orbit, at an epoch of 19 December 1966, it had a perigee of 188 kilometres (117 mi), an apogee of 280 kilometres (170 mi), an inclination of 64.6°, and an orbital period of 89.4 minutes.[3] After eight days in orbit, Kosmos 136 was deorbited, with its return capsule descending under parachute, landing at 06:00 GMT on 27 December 1966, and recovered by Soviet force.[2]

YouTube Encyclopedic

  • 1/5
    20 641
    44 954
    48 610
    32 525
    14 391
  • 136 Wie Entstehen Gasplaneten
  • The Most Massive Star Known | R136a1
  • Las estrellas más masivas que podemos ver a simple vista - El Cosmos
  • Liebe radikal - Wie deine Beziehungen erblühen, wenn du dich existentiell einlässt - Folge 138
  • Das Licht und seine Geheimnisse | Deutsch lernen mit Videos



  1. ^ a b "Cosmos 136: Display 1966-115A". NASA. 27 February 2020. Retrieved 2 April 2020. This article incorporates text from this source, which is in the public domain.
  2. ^ a b Christie, Robert. "Zenit Satellites - Zenit-2 variant". Retrieved 5 January 2014.
  3. ^ a b "Cosmos 136: Trajectory 1966-115A". NASA. 27 February 2020. Retrieved 2 April 2020.
  4. ^ Krebs, Gunter. "Zenit-2 (11F61)". Gunter's Space Page. Archived from the original on 31 December 2011. Retrieved 5 January 2014.
  5. ^ Wade, Mark. "Zenit-2". Encyclopedia Astronautica. Archived from the original on 21 April 2012. Retrieved 5 January 2014.
  6. ^ Wade, Mark. "Vostok 8A92". Encyclopedia Astronautica. Archived from the original on 22 August 2016. Retrieved 5 January 2014.
  7. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 5 January 2014.
This page was last edited on 28 January 2021, at 15:34
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.