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IRS-1E

Launch Date:20.09.1993

irs1e

IRS-1E satellite is derived from the engineering model of IRS-1A flown on the first developmental flight of Polar Satellite Launch Vehicle (PSLV). The satellite carried a Monocular Electro-Optical Stereo Scanner developed by DLR, Germany, and a LISS-I camera similar to that on IRS-1A. The satellite could not be placed into orbit by the PSLV-D1

Mission Operational Remote Sensing
Orbit Not Realised
Orbit Inclination -
Lift-off Mass 846 kg
Orbit Period -
Local Time of Equator crossing -
Repetitivity -
Payloads

LISS-1: 65.5 m resolution, 134 km swath, 7 bit radiometry; 4 bands (B1: 0.45-0.52 µm; B2: 0.52-0.59 µm; B3: 0.62-0.68 µm; B4: 0.77-0.86 µm)

Monocular Electro-Optical Stereo Scanner (MEOSS) – 50.3 m resolution along track; 463 km swath; 8 bit radiometry

Attitude and Orbit Control 3-axis body stabilized with 4 reaction wheels and magnetic torquers
Power Solar Array generating 415 W backed by 2 Ni-Cd batteries of 40 AH capacities each
Launch date September 20, 1993
Launch site SHAR Centre, Sriharikota, India
Launch vehicle PSLV-D1
Mission life -
Orbital life Not realized
    Site last updated: Monday 11 December 2017
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