KazEOSat 2

KazEOSat-2
Spacecraft properties

Mission type	Remote sensing
Operator	Kazakhstan Gharysh Sapary (KGS)
COSPAR ID	2014-033A^[1]
Website	kazcosmos.gov.kz/en/news/200614.html
Mission duration	3 years

Bus	SSTL-150
Manufacturer	EADS Astrium
Launch mass	~177 kilograms (390 lb)
Dimensions	700 by 800 by 900 millimetres (28 in × 31 in × 35 in)
Power	150 watts

Start of mission
Launch date	June 19, 2014, 19:11 (2014-06-19UTC19:11Z) UTC
Rocket	Dnepr
Launch site	Dombarovsky 370/13
Contractor	Kosmotras

Orbital parameters
Reference system	Geocentric
Regime	Sun-Synchronous
Perigee	630 kilometres (390 mi)
Apogee	630 kilometres (390 mi)
Inclination	97.9 degrees

KazEOSat is a remote sensing Earth observation satellite built for the Kazakhstan Gharysh Sapary under an agreement with EADS Astrium and SSTL, a satellite manufacturing companies in France and England, respectively. The earth observation satellite was designed and developed by EADS Astrium, and represent 11th launch of SSTL-150 bus, first launched in 2005.^[2]

References

↑ "KazEOSat 2 Gunters space page". Retrieved June 24, 2014.
↑ http://space.skyrocket.de/doc_sat/sstl_150.htm

External links

KAzEOSat 2 launch announcement

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Payloads are separated by bullets ( · ), launches by pipes ( \| ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).

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