HySIS

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General

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

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Specifications

Prime contractor	ISRO
Platform	IMS 2
Mass at launch	730 kg
Dry mass
Dimension
Solar array
Stabilization
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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