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Intelsat 802
Mission type Communications
Operator Intelsat
COSPAR ID 1997-031A Edit this at Wikidata
SATCAT no.24846
Mission duration14 years
Spacecraft properties
Spacecraft type AS-7000
Manufacturer Lockheed Martin
Launch mass3,447 kilograms (7,599 lb)
Start of mission
Launch dateJune 25, 1997, 01:07:42 (1997-06-25UTC01:07:42Z) UTC [1]
Rocket Ariane-44P H10-3
Launch site Kourou ELA-2
Contractor Arianespace
End of mission
DeactivatedOctober 2010 (2010-11)
Orbital parameters
Reference system Geocentric
Regime Geostationary
Now supersynchronous
Longitude174° W (original)
55.6° W (current) [2]
Semi-major axis427,820 kilometres (265,840 mi) [2]
Perigee altitude362,922 kilometres (225,509 mi) [2]
Apogee altitude365,299 kilometres (226,986 mi) [2]
Inclination4.9 degrees [2]
Period1,467.8 minutes [2]
EpochMay 5, 2017 [2]
Transponders
Band38 C Band, 6 Ku band
Coverage area Europe, Africa, Asia
Intelsat 8
 

Intelsat 802 was a communications satellite operated by Intelsat. Launched in 1997 it was operated in geostationary orbit at a longitude of 174 degrees west for around fourteen years.

Satellite

The second of six Intelsat VIII satellites to be launched, Intelsat 802 was built by Lockheed Martin. It was a 3,447-kilogram (7,599 lb) spacecraft. The satellite carried a 2x LEROS-1B apogee motor for propulsion and was equipped with 38 C Band transponders and 6 Ku band transponders, powered by 2 solar cells more batteries. [3] It was designed for a fourteen-year service life. [4]

Launch

The launch of Intelsat 802 made use of an Ariane 4 rocket flying from Guiana Space Centre, Kourou, French Guiana. The launch took place at 01:07 UTC on June 25, 1997, with the spacecraft entering a geosynchronous transfer orbit. [1] Intelsat 802 subsequently fired its apogee motor to achieve geostationary orbit.

See also

References

  1. ^ a b McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved May 5, 2017.
  2. ^ a b c d e f g "INTELSAT 801". N2YO. Retrieved May 5, 2017.
  3. ^ Wade, Mark. "Intelsat". Encyclopedia Astronautica. Retrieved July 8, 2022.
  4. ^ Krebs, Gunter. "Intelsat-8 (801, 802, 803, 804) / NSS 803 → NSS 5". Gunter's Space Page. Retrieved May 5, 2017.