Carried two TV cameras, one in visible and the other in near-infrared band, and
a 3-frequency passive microwave radiometer. The cameras malfunctioned.
Spacecraft data:
Prime manufacturer
Platform
Operator
Mass at launch
442 kg
Dry Mass
kg
Basic shape
Dimension (m)
Equipment
TVcameras, three band Microwave Radiometer (SAMIR)
Solar array
none, solar cells
Stabilization
Spin stabilized (spin axis controlled)
Communication
VHF band
DC power
47 W
Design lifetime
10 yrs
End of life
Re-entered date
17 Feb 1989
Description:
The First Experimental Remote Sensing Satellite built in India.
The onboard TV camera sent imageries which we reused in the field of Hydrology and Forestry. SAMIR sent rich scientific
data which were used for oceanographic studies.