Göktürk 2

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Göktürk 2
Type: Reconnaissance satellite
Country: TurkeyTurkey Turkey
COSPAR-ID : 2012-073A
Mission dates
Dimensions: 450 kg
Begin: December 18, 2012, 3:13 pm UTC
Starting place: Jiuquan
Launcher: Long March 2D
Flight duration: 5 years
Orbit data
Rotation time : 98.3 min
Orbit inclination : 98.2 °
Apogee height 697 km
Perigee height 676 km

Göktürk 2 is a reconnaissance satellite that was largely developed and built in Turkey .

It was brought into sun-synchronous orbit on December 18, 2012 at 16:13 CET with a Long March 2D launcher from the Chinese rocket launch site in Jiuquan .

The actual predecessor Göktürk 1 was only launched in December 2016. A contract between Telespazio and Thales Alenia Space, on the one hand, and the Turkish Ministry of Defense, on the other hand, to build a reconnaissance satellite with a resolution of less than one meter was signed in December 2008. Telespazio was supposed to involve local Turkish companies in the development of the satellite systems and a ground segment.

The three-axis stabilized satellite is equipped with a multispectral camera built in South Korea and has a resolution of 2.5 m panchromatic , 10 m multispectral and 20 m in the near infrared range as well as a swath width of 20 km. The storage capacity on board the satellite is 15 GB. The solar cell boom comes from the German company SpaceTech from Immenstaad. Göktürk 2 was built for the Turkish Ministry of Defense and has a planned lifespan of five years. In addition to military tasks, it should also serve civil tasks such as environmental and disaster protection.

Web links

Individual evidence

  1. Railway data according to GOKTURK 2. n2yo, April 2, 2013, accessed on April 2, 2013 (English).
  2. ^ Günther Glatzel: Turkish reconnaissance satellite launched. raumfahrer.net, December 20, 2012, accessed on December 21, 2012 .
  3. NASASpaceFlight.com: China end 2012 with Long March 2D launch of Göktürk-2