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From Wikipedia, the free encyclopedia

Mission typeRemote sensing
OperatorDeimos Imaging
COSPAR ID2014-033D
SATCAT no.40013Edit this on Wikidata
Mission duration7 years
Spacecraft properties
ManufacturerSatrec Initiative
Launch mass≈310 kilograms (680 lb)
Dimensions1,200 by 1,200 millimetres (47 in × 47 in)
Power330 watts
Start of mission
Launch dateJune 19, 2014, 19:11 (2014-06-19UTC19:11Z) UTC
Launch siteDombarovsky 370/13
Orbital parameters
Reference systemGeocentric
Perigee altitude597 kilometres (371 mi)
Apogee altitude617 kilometres (383 mi)
Inclination97.9 degrees
Epoch27 June 2014[1]
Main camera
WavelengthsPan: 420-720 nm
MS1: 420-510 nm (Blue)
MS2: 510-580 nm (Green)
MS3: 600-720 nm (Red)
MS4: 760-890 nm (Near Infrared)
Resolution0.75 metres (2 ft 6 in) (Pan)
5 metres (16 ft) (MS)

Deimos-2 is a Spanish remote sensing Earth observation satellite built for Elecnor Deimos under an agreement with Satrec Initiative, a satellite manufacturing company in South Korea.

The Earth observation system was developed by Elecnor Deimos, who managed the engineering, ground segment, integration, tests, launch contract and LEOP, in collaboration with Satrec Initiative, who provided the platform and the payload.[2] The platform is based on DubaiSat-2 launched in 2013, with a larger battery pack intended to last for at least 7 years.[3] The satellite was purchased by Urthecast in 2015, together with Deimos-1 and Deimos Imaging, the division of Elecnor Deimos that was in charge of the operation of both satellites.[4]

Deimos-2 is currently property of Deimos Imaging, who operates it and commercialises its data.

YouTube Encyclopedic

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  • The Moons of Mars Explained -- Phobos & Deimos MM#2


See also


  1. ^ McDowell, Jonathan. "SATCAT". Jonathan's Space Pages. Retrieved 3 May 2018.
  2. ^ "DEIMOS-2".
  3. ^ (Admin), Roger Longhorn. "GSDI - Home" (PDF).
  4. ^ "Urthecast Buying Deimos' Imaging Division and its 2 Satellites". 23 June 2015.

External links

This page was last edited on 21 December 2020, at 17:52
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