Intelsat 801 Explained

Intelsat 801
Mission Type:Communications
Operator:Intelsat
Cospar Id:1997-009A
Satcat:24742
Mission Duration:16 years
Spacecraft Bus:AS-7000
Manufacturer:Lockheed Martin
Dry Mass:1601kg (3,530lb)
Launch Mass:3245kg (7,154lb)
Dimensions:2.46×
Power:6400 W
Launch Date: UTC[1]
Launch Rocket:Ariane-44P H10-3
Launch Site:Kourou ELA-2
Launch Contractor:Arianespace
Disposal Type:Decommissioned
Orbit Reference:Geocentric
Orbit Regime:Geostationary
Orbit Periapsis:35772km (22,228miles)
Orbit Apoapsis:35798km (22,244miles)
Orbit Inclination:0.1°
Orbit Period:1,436.1 minutes
Apsis:gee
Trans Frequency:Uplink: 14.00-14.50 GHz
Downlink: 10.95-11.2 GHz, 11.7-11.95 GHz, 12.5-12.75 GHz and 11.45-11.70 GHz
Trans Coverage:Europe, Africa, Asia
Programme:Intelsat 8
Previous Mission:Intelsat 7-F9 (Intelsat VII)
Next Mission:Intelsat 802

Intelsat 801 is a geosynchronous communications spacecraft that was launched on March 01, 1997 by an Ariane 44L rocket from Kourou in French Guiana to provide voice and video communications to the member countries in that consortium after parking at 174° E longitude. It carries 38 C Band and 6 Ku Band transponders. It was built for US$76 million, launched for US$86 million and insured for US$27 million.[2] [3]

Specifications

See also

Notes and References

  1. Web site: Intelsat-8 (801, 802, 803, 804) / NSS 803 → NSS 5 . Gunter . Krebs . May 4, 2017.
  2. Web site: Intelsat 801 . NASA . GSFC . May 5, 2017.
  3. Web site: Intelsat 801 . TBS . May 5, 2017.