INSAT-2DT

{{Short description|Decommissioned Indian geostationary communications satellite}}

{{Infobox spaceflight

| name = Arabsat-1C → INSAT-2DT

| image =

| image_caption =

| mission_type = Communication

| operator = ArabsatINSAT

| website =

| COSPAR_ID = 1992-010B

| SATCAT = 21894

| mission_duration = 7 years (planned)
12¾ years (achieved)

| spacecraft_bus = Spacebus 100

| manufacturer = Aérospatiale/MBB

| dry_mass =

| launch_mass = {{convert|1360|kg}}

| power =

| launch_date = {{start-date|26 February 1992, 23:58:10|timezone=yes}} UTC

| launch_rocket = Ariane 44L

| launch_site = Kourou ELA-2

| launch_contractor = Arianespace

| entered_service =

| disposal_type = Decommissioned

| deactivated = {{end-date|October 2004}}

| orbit_epoch =

| orbit_reference = Geocentric

| orbit_regime = Geostationary

| orbit_periapsis =

| orbit_apoapsis =

| orbit_inclination =

| orbit_period = 24 hours

| orbit_longitude = 31° East
55° East
82.5° East

| orbit_slot =

| apsis = gee

| trans_band = 2 E/F-band
25 G/H-Band

| trans_frequency =

| trans_bandwidth =

| trans_capacity =

| trans_coverage =

| trans_TWTA =

| trans_EIRP =

| trans_HPBW =

}}

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

Launched in 1992 as Arabsat-1C, it was operated at 31° East longitude in geostationary orbit,{{cite web |url=http://www.astronautix.com/project/arabsat.htm |title=Arabsat |last=Wade |first=Mark |publisher=Encyclopedia Astronautica |access-date=2009-07-05 |url-status=dead |archive-url=https://web.archive.org/web/20090331213805/http://www.astronautix.com/project/arabsat.htm |archive-date=2009-03-31 }} 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 {{convert|1170|kg}}, and an expected operational lifespan of seven years.{{cite web |url=http://space.skyrocket.de/doc_sdat/arabsat-1a.htm |title=Arabsat 1A, 1B, 1C / Insat 2DT |last=Krebs |first=Gunter |publisher=Gunter's Space Page |access-date=2009-07-05}}

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.{{cite web |url=http://planet4589.org/space/log/launchlog.txt |title=Launch Log |last=McDowell |first=Jonathan |publisher=Jonathan's Space Page |access-date=2009-07-05}} It was the final Spacebus 100 satellite to be launched.

Indian operations

In November 1997, Arabsat-1C was sold to India as INSAT-2DT.{{cite web |url=http://www.tbs-satellite.com/tse/online/sat_arabsat_1c.html |title=Arabsat 1C |publisher=TSE |access-date=2009-07-05}} 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.{{cite web |url=http://www.tbs-satellite.com/tse/online/sat_insat_2d.html |title=INSAT-2D |publisher=TSE |access-date=2009-07-05}} It remained at 55°E until August 2003, when it was moved to 85.2°E, arriving in November.{{cite web |url=http://www.tbs-satellite.com/tse/online/sat_insat_2r.html |title=INSAT-2R |publisher=TSE |access-date=2009-07-05}} 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.

See also

{{Portal|Spaceflight}}

References