Official name INTELSAT 805
Alternative name Intelsat 805
Cospar ID 1998-037A
Norad ID 25371
Launch date 1998-06-18
Launch site AFETR
Launch vehicle Atlas-2AS
Country/Organization International, Netherlands (NSS)
Type application Communication
Operator Intelsat / New Skies (NSS)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1447.55
Inclination (deg) 5.95
Perigee (km) 35963
Apogee (km) 36058
Eccentricity 0.00131905971869316
Mean motion (revs. per day) 0.994784290698076
Semi-Major axis (km) 42388.635
Raan (deg) 74.4129
Arg of perigee (deg) 125.7149
Shape Hex Poly + 2 Pan
Mass (kg) 1932.61
Height (m) 5.19
Width (m) 2.2
Depth (m) 2.2
Span (m^2) 10.8
Lifetime 14-17 years, depending on the launch vehicle
Contractors Lockheed Martin
Equipment 28 C-band transponders, 3 Ku-band transponders
Propulsion 2 × LEROS-1b
Configuration AS-7000
Power 2 deployable solar arrays, batteries

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.

This deployment of Intelsat 805 was originally scheduled to use a Chinese CZ-3B rocket. However, Intelsat bailed out of that plan after losing one of its satellites in a 1996 catastrophic launch explosion of a CZ-3B booster.

In January 2020 Intelsat 805 was put into a graveyard orbit and was passivated.

Satellite COSPAR Date LS Launch Vehicle Remarks
NSS 806 (INTELSAT 806) 1998-014A 1998-02-28 AFETR Atlas-2AS
INTELSAT 805 1998-037A 1998-06-18 AFETR Atlas-2AS