Rasat

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General

Designation	37791 / 11044D
Launch date	17 Aug 2011
Country of origin	Turkey
Mission	Remote sensing
Perigee/Apogee	675/705 km
Inclination	98.3°
Period	98.4 min
Launch vehicle	Dnepr #17

First Earth observation satellite built in Turkey. 95 kg

Has a high-resolution (7.6 m) optical imaging system (Korean-built) and new modules developed by Turkish engineers.

Owned by Space Technologies Research Institute of Turkey's Scientific


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Technical data

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Specifications

Prime contractor
Platform
Mass at launch	93 kg
Dry mass
Dimension
Solar array
Stabilization
DC power
Design lifetime	3 years

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