Sputnik 11A59

In-active

Energia (OKB-1)

Dec. 1, 1963

Description

An early Russian rocket designed by Sergei Korolev in the Soviet Union

Specifications
  • Stages
    1
  • Length
    30.0 m
  • Diameter
    2.99 m
  • Fairing Diameter
    2.99 m
  • Launch Mass
    277 T
  • Thrust
    3999 kN
Family
  • Name
    Sputnik 11A59
  • Family
  • Variant
    11A59
  • Alias
  • Full Name
    Sputnik 11A59
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    1400 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Energia

Government
None
OKB-1 1946

None

Sputnik 11A59 | Polyot-2

Energia | Russia
Baikonur Cosmodrome, Republic of Kazakhstan
April 12, 1964, 9:30 a.m.
Status: Launch Successful
Mission:

Polyot 2 (I1) was a mission to test the propulsion of the I2P coorbital ASAT satellite. It did not conduct any interception maneuveres.

Low Earth Orbit
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Sputnik 11A59 | Polyot

Energia | Russia
Baikonur Cosmodrome, Republic of Kazakhstan
Nov. 1, 1963, 8:56 a.m.
Status: Launch Successful
Mission:

Polyot 1 (I1) was a mission to test the propulsion of the I2P coorbital ASAT satellite.

Low Earth Orbit
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Long March 6A
Success
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FLTA005 (Noise of Summer)
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Long March 7A
Success
6 days, 17 hours ago
ChinaSat 3A
201 - Wenchang Space Launch Site, People's Republic of China

Chinese communication geostationary satellite for unknown purposes.