NamesEarth Remote Observation System-A
Mission typeEarth observation
OperatorImageSat International
COSPAR ID2000-079A
SATCAT no.26631
Mission duration10 years (planned)
16.5 years (achieved)
Spacecraft properties
Spacecraft typeOfeq-3
ManufacturerIsrael Aerospace Industries
Launch mass260 kg (570 lb)
Dimensions2.3 m in height
1.2 m in diameter
Power450 watts
Start of mission
Launch date5 December 2000, 12:32 UTC[2]
Launch siteSvobodny Cosmodrome,
Launch Complex-5
ContractorMoscow Institute of Thermal Technology
End of mission
Last contactMay 2016 [3]
Decay date7 July 2016 [4]
Orbital parameters
Reference systemGeocentric orbit[5]
RegimeLow Earth orbit
Perigee altitude490 km (300 mi)
Apogee altitude565 km (351 mi)
Period94.60 minutes

The Earth Remote Observation System-A (EROS-A or EROS-A1) was part of the EROS family of Israeli commercial Earth observation satellites, designed and manufactured by Israel Aircraft Industries (IAI).[6] This was the first satellite in the series. The satellite was owned and operated by ImageSat International, ImageSat International N.V. (ISI) headquartered at Limassol, Cyprus, and incorporated in the Netherlands Antilles, Cayman Islands.[7]


The EROS A was launched on 5 December 2000, at 12:32 UTC,[2] from Svobodny Cosmodrome, Launch Complex-5 in eastern Siberia.[7]

Satellite description

The satellite was 1.2 m in diameter, 2.3 m in height. It weighed 260 kg at launch.[7] The design was based on the military reconnaissance satellite Ofeq-3, which was previously built, also by Israel Aerospace Industries (IAI) for Israeli government use.

Control systems

The satellite was equipped with a three-axis stabilized and a four reaction wheels actuator. The satellite is also equipped with horizon sensors, sun sensors, gyroscopes and magnetometer for altitude determination.[3]

Ground communication systems

The satellite is equipped with a 70 Mbit/s imagery link, a 15 kbit/s maintenance downlink, and a 15 kbit/s command uplink.[8]


The satellite always crosses the equator at 10:00 am local time. Future satellites were planned to extend the time dimension to vary the crossing time between mid-morning and mid after. This will allow it to compensate for poor visibility conditions arising from clouds at different altitudes. While the satellite's primary purpose is agricultural engineers, planners and other professionals who need detailed pictures of different places in the world, it can also be used for various other applications. The satellite provides commercial images with an optical resolution of 1.8 metres using. It has optical resolution capabilities of up to 1.2 meters. The satellite can be temporarily controlled by a customer when it passes over the areas of interest. This is used to allow the client privacy without the operator knowing what's being looked at. This capability, however, is not allowed over the State of Israel by the Israeli government.

The satellite increased its orbital altitude for the last time on 24 April 2012 and reentered on 7 July 2016.[1]

See also


  1. ^ a b "EROS-A1, A2". Gunter's Space Page. 7 July 2020. Retrieved 9 May 2021.
  2. ^ a b "Launch Log". Jonathan's Space Report. 14 March 2021. Retrieved 9 May 2021.
  3. ^ a b "EROS A". Apollo Mapping. Retrieved 9 May 2021.
  4. ^ Peat, Chris (21 November 2013). "EROS-A1 - Orbite". Heavens Above. Retrieved 9 May 2021.
  5. ^ "Trajectory:EROS-A1 2000-079A". NASA. 27 April 2021. Retrieved 9 May 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  6. ^ "Serbia Settlement IAI Bond Purchase Boost Fortunes of Israel's ImageSat". SpaceNews. 28 January 2011. Retrieved 9 May 2021.
  7. ^ a b c "EROS-A (Earth Remote Observation System-A)". ESA Earth Observation Portal. Retrieved 9 May 2021.
  8. ^ A., Klein (16–20 September 1996). "Flight Operations Engineering for the Earth Resource Spacecraft EROS-A". NASA. Retrieved 9 May 2021. Public Domain This article incorporates text from this source, which is in the public domain.