Official name EROS A1
Alternative name EROS A1
Cospar ID 2000-079A
Norad ID 26631
Launch date 2000-12-05
Launch site SVOB
Launch vehicle Start-1
Country/Organization Israel
Type application Earth observation
Operator ImageSat International (ISI)
RCS size MEDIUM
Decay date 2016-07-07
Shape Taper Cyl + 2 Pan
Mass (kg) 250
Diameter (m) 1.2
Height (m) 2.3
Span (m^2) 4
Lifetime 6 - 10 years
Contractors IAI
Equipment ?
Propulsion ?
Configuration OPSAT-1000 Bus
Power 2 deployable fixed solar arrays, batteries

EROS A (Earth Resources Observation Systems A) is the first in a constellation of sun-synchronous, polar-orbiting satellites that ImageSat plans to deploy during this decade.

EROS A is based on the military Ofeq 3 and 4 type satellites, which weighed 250 kg at launch, orbits at an altitude of 480 km in a sun-synchronous orbit ensuring that all images are taken at the same local time at each pass. EROS A is equipped with a camera whose focal plane of CCD (Charge Coupled Device) detectors produce a standard image resolution of 1.8 meters at a swath of 13.5 km at Nadir (perpendicular to the surface), and sub-meter resolution using hypersampling techniques. The data transmission rate is 70 Mbit/s, and the anticipated lifespan of the EROS A satellite is six to ten years. ImageSat expect it to work for 14 years.

EROS A was launched on 5 December 2000 on a Start-1 booster. The satellite performed its last orbit rising manoeuvre on 24 April 2012 and finally reentered on 7 July 2016.

Satellite COSPAR Date LS Launch Vehicle Remarks
EROS A1 2000-079A 2000-12-05 SVOB Start-1