Yamal 402

Russia

Spacecraft nº:

Russian spacecraft nº:


Launch data:

Designation 39022 / 12070A
Launch date 08 Dec 2012 - 13:13 UT
Launch site Baikonur, LC-39/200
Launch vehicle  Proton-M/Briz-M
Mission Com.: Communication
Geostationary orbit:
Perigee / Apogee 35784 x 35789 km
Eccentricity 5,93E-05
Inclination 0.06 deg
Period 1436.11 min

Partial failure


Spacecraft data:

Prime manufacturer Thales Alenia Space (FR)
Platform Spacebus-4000C3
Operator Gazprom Space Systems
Mass at launch  5250 kg (4463?)
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment 46 Ku-band transponders
Solar array 2 deployable solar arrays
Stabilization  
Propulsion S400, 4 SPT-100 plasma thrusters
DC power  
Design lifetime  15 yrs (planned), 11 yrs (expected after launch failure) - still active

Location:

DatePositionRemarks
 31 May 2013  55° E 



Description:

Mission details:

External links:


Ref.: #7(JR671-672), #14, #211, #226, #228 - update: 20.02.13 Home