INSAT-2DT

From Bharatpedia, an open encyclopedia
Information red.svg
Scan the QR code to donate via UPI
Dear reader, We need your support to keep the flame of knowledge burning bright! Our hosting server bill is due on June 1st, and without your help, Bharatpedia faces the risk of shutdown. We've come a long way together in exploring and celebrating our rich heritage. Now, let's unite to ensure Bharatpedia continues to be a beacon of knowledge for generations to come. Every contribution, big or small, makes a difference. Together, let's preserve and share the essence of Bharat.

Thank you for being part of the Bharatpedia family!
Please scan the QR code on the right click here to donate.

0%

   

transparency: ₹0 raised out of ₹100,000 (0 supporter)


Arabsat-1C → INSAT-2DT
Mission typeCommunication
OperatorArabsatINSAT
COSPAR ID1992-010B
SATCAT no.21894
Mission duration7 years (planned)
12¾ years (achieved)
Spacecraft properties
BusSpacebus 100
ManufacturerAérospatiale/MBB[1]
Launch mass1,360 kilograms (3,000 lb)
Start of mission
Launch date26 February 1992, 23:58:10 (1992-02-26UTC23:58:10Z) UTC
RocketAriane 44L
Launch siteKourou ELA-2
ContractorArianespace
End of mission
DisposalDecommissioned
DeactivatedOctober 2004 (2004-11)
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude31° East
55° East
82.5° East
Period24 hours
Transponders
Band2 E/F-band
25 G/H-Band
 

INSAT-2DT, previously Arabsat-1C and also known as INSAT-2R, was a Saudi Arabian and subsequently Indian communications satellite which was operated initially by Arabsat, and then by the Indian National Satellite System.

Launch and Arabsat service[edit]

Launched in 1992 as Arabsat-1C, it was operated at 31° East longitude in geostationary orbit,[2] from where it was used to provide communication services to the Arab States. It was constructed by Aérospatiale, based on the Spacebus 100 satellite bus, and carried two NATO E/F-band (IEEE S band) and 25 NATO G/H-Band (IEEE C band) transponders. At launch, it had a mass of 1,170 kilograms (2,580 lb), and an expected operational lifespan of seven years.[1]

It was launched by Arianespace using an Ariane 4 rocket in the 44L configuration, flying from ELA-2 at the Guiana Space Centre in Kourou. The launch took place at 22:58:10 UTC on 26 February 1992.[3] It was the final Spacebus 100 satellite to be launched.

Indian operations[edit]

In November 1997, Arabsat-1C was sold to India as INSAT-2DT.[4] In December, it was moved to a new slot at 55°E longitude, where it replaced the INSAT-2D satellite which had failed in orbit.[5] It remained at 55°E until August 2003, when it was moved to 85.2°E, arriving in November.[6] By the time of its departure from 55°E, its orbital inclination had increased somewhat.

INSAT-2DT remained at 85.2°E until October 2004, when it was retired from service and placed into a graveyard orbit.[6]

See also[edit]

References[edit]

  1. 1.0 1.1 Krebs, Gunter. "Arabsat 1A, 1B, 1C / Insat 2DT". Gunter's Space Page. Retrieved 2009-07-05.
  2. Wade, Mark. "Arabsat". Encyclopedia Astronautica. Archived from the original on 2009-03-31. Retrieved 2009-07-05.
  3. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-07-05.
  4. "Arabsat 1C". TSE. Retrieved 2009-07-05.
  5. "INSAT-2D". TSE. Retrieved 2009-07-05.
  6. 6.0 6.1 "INSAT-2R". TSE. Retrieved 2009-07-05.

Template:INSAT Satellites

Template:Orbital launches in 1992