Intelsat 8 Series (801, 803, 802, 804, 805A, 806A)
(to Western Hemisphere, Eastern Hemisphere
, Footprints by Dish Size)

This page was originally on the Intelsat website however they scrapped it when
they made their current website so I have reproduced it for your research convenience.

The INTELSAT 8 Satellites
As of 1 June 1998, three INTELSAT VIII satellites are in service in the Atlantic, Indian and Pacific Ocean Regions. One INTELSAT VIII/A satellite (INTELSAT 805) is due to be launched in June of 1998 for deployment in the Atlantic Ocean Region (AOR) at 304.5°E.
INTELSAT 801 @ 328.5°E AOR
INTELSAT 802 @ 174°E POR
INTELSAT 804 @ 64°E IOR
INTELSAT 805 @ 304.5°E* AOR
* Future planned spacecraft.
Capacity
INTELSAT VIII: 22,500 two-way telephone circuits and three TV channels; up to 112,500 two-way telephone circuits with the use of digital circuit multiplication equipment (DCME).
Lifetime
14-17 years, depending on the launch vehicle.
Launch Vehicles
Arianespace Ariane 44P
ILS International Launch Services Atlas II AS
Launches

Spacecraft
Launch
Vehicle
Spacecraft
Delivery
Launch
Window/Date
Launch
Result
INTELSAT 801 Ariane 44P 30 Dec. 1996 27 Feb. 1997 Success
INTELSAT 802 Ariane 44P 29 April 1997 25 Jun. 1997 Success
INTELSAT 804 Ariane 42L 21 Oct. 1997 21 Dec. 1997 Success
INTELSAT 805 Atlas IIAS 15 May 1998 18 Jun. 1998 n/a
Note:
INTELSAT VIII/A launch window represents INTELSAT's best estimate at this time and is being coordinated with launch services contractor
.
Capabilities
Transponders INTELSAT VIII INTELSAT VIII/A
C-band Transponders 38 28
Ku-band Transponders 06 3
Total 44 31
The INTELSAT VIII-VIII/A series has been designed to meet the needs of INTELSAT users throughout the system for improved C-band coverage and service. These spacecraft will incorporate six-fold C-band frequency reuse, two-fold frequency reuse of expanded C-band capacity, and the highest C-band power level ever for an INTELSAT satellite. Consequently, INTELSAT VIII will provide significantly more C-band capacity for public switched telephony and INTELSAT Business Service, better quality for video services, and encourage new international VSAT applications.
Other salient features of INTELSAT VIII satellites include:
  • Two independently steerable Ku-band spot beams which can be pointed anywhere on the surface of the earth that is visible from the spacecraft in geosynchronous orbit.
  • Interconnected operation between C- and Ku-bands.
  • Expanded SNG (satellite news gathering) service provided by the capability to connect spot beams to global beams, including a return path for small Ku-band transportable SNG stations for voice/data communications.
  • Compatibility with INTELSAT VII/VII-A satellites to facilitate operation with and transition to INTELSAT VIII spacecraft.
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