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Designation 43719 / 18096A
Launch date 29 Nov 2018
Country of origin India
Mission IR Remote sensing
Perigee/Apogee 630 km
Inclination 98°
Period 97.5 min
Launch vehicle PSLV #46

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Technical data


Prime contractor ISRO
Platform IMS 2
Mass at launch 730 kg
Dry mass  
Solar array  
DC power  
Design lifetime 5 years

Two payloads: one to capture images in the visible near-infrared (VNIR) range of the light spectrum and another in the shortwave infrared (SWIR) range.

The optical imaging detector array chip in the HySIS satellite has been designed by Isro's Ahmedabad-based Space Applications Centre and manufactured by its electronic arm, Semi-Conductor Laboratory, Chandigarh.

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