AB
picture credit: NASA
NamesGranat
Astron 2
Mission typeAstronomy
OperatorSoviet space program
Roscosmos
COSPAR ID1989-096A
SATCAT no.20352
Websitehea.iki.rssi.ru
Mission duration8 years, 11 months and 26 days
Spacecraft properties
Bus4MV
ManufacturerNPO Lavochkin1
Launch mass~4,400 kg (9,700 lb)
Payload mass~2,300 kg (5,100 lb)
Dimensions4.0 × 2.5 m (13.1 × 8.2 ft)
Power400 W
Start of mission
Launch date20:20, December 1, 1989 (UTC)2
RocketProton-K/D-13
Launch siteBaikonur 200/40
End of mission
DisposalDeorbited
Last contact27 November 1998
Decay dateMay 25, 19992
Orbital parameters
Reference systemGeocentric1
RegimeHighly elliptical
Eccentricity0.92193
Perigee altitude1,760 kilometres (1,090 mi)4
Apogee altitude202,480 kilometres (125,820 mi)
Inclination51.9 degrees
Period5,880 minutes
Epoch01 December 1989
Main telescope
NameSIGMA
TypeCoded mask
Diameter1.2 metres (3.9 ft)
Focal length2.5 metres (8.2 ft)
Collecting area800 cm (120 sq in)
WavelengthsX-ray to γ-ray, 1–620 pm (2 keV – 1.3 MeV)
Instruments

International Astrophysical Observatory

(echo:: @ )

Footnotes

  1. “Granat X-ray and Gamma-ray Observatory”. The Federation of American Scientists. Archived from the original on 2007-02-06. Retrieved 2007-12-06. 2

  2. “1999 Reentries” (PDF). The Aerospace Corporation, Center for Orbital and Reentry Debris Studies. Archived from the original (PDF) on 2005-01-22. Retrieved 2007-12-06. 2

  3. “GRANAT”. NASA HEASARC. Archived from the original on 2016-03-06. Retrieved 2007-12-05.

  4. (in Russian) N.G. Kuleshova, I.D. Tserenin, A.I. Sheikhet, from NPO Lavochkin, Orbital Astrophysical Observatory “Granat”: Problems of Control Archived 2007-10-31 at the Wayback Machine, Zemlya i Vselennaya, 1994, no. 2. Only four rows from a table of twenty used here.