Göktürk 2 2

Turkey

Spacecraft nr:

Turkish spacecraft nr: 9


Launch data:

Designation 39030 / 12073A
Launch date 18 Dec 2012 - 16:12UT
Launch site Jiuquan, SLS-2
Launch vehicle  CZ-2D
Mission Mil.: Earth observing
Sun-synchronous Earth orbit:
Perigee / Apogee 669 x 690 km
Eccentricity 1,49E-03
Inclination 98.16 deg
Period 98.35 min


Spacecraft data:

Prime manufacturer Turkish Aerospace Industries, Inc. (TAI)
Platform 
Operator Turkish Ministry of Defence
Mass at launch  450 kg (409?)
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment 
Image Storage capacity > 15 Gbit
Solar array 
Stabilization  3 deployable fixed solar arrays
Propulsion 
DC power  
Design lifetime  5 yrs - still active

Gokturk satellite - Credit: Turkish Defence






Description:

Mission details:

External links:


Ref.: #7(JR672), #226, #228, #http://www.trdefence.com - update: 22.01.14 Home