Inmarsat-4 F3 Explained

Inmarsat-4 F3
Operator:Inmarsat
Spacecraft Bus:Eurostar E3000
Manufacturer:EADS Astrium
Launch Mass:5960kg (13,140lb)
Launch Site:Baikonur 200/39
Entered Service:7 January 2009
Orbit Reference:Geocentric
Orbit Regime:Geostationary
Orbit Longitude:98° West
Apsis:gee

Inmarsat-4 F3 is a communications I-4 satellite operated by the British satellite operator Inmarsat. It was launched into a geosynchronous orbit at 22:43 GMT on 18 August 2008,[1] by a Proton-M/Briz-M Enhanced carrier rocket. It is currently located at 97.65° West longitude, providing coverage of the Americas.[2] It entered service on 7 January 2009.

Like the earlier Inmarsat-4 F1 and F2 satellites, Inmarsat-4 F3 was constructed by EADS Astrium, using a Eurostar E3000 bus. It has a mass of 5,960 kilograms, and is expected to operate for 13 years.[3] It was originally slated for launch using an Atlas V 531, but was transferred to Proton due to a large backlog of Atlas launches.

In the United States, Inmarsat ground stations are licensed to operate at 1525-1559 MHz and 1626.5-1660.5 MHz. The 1544-1545 MHz and 1645.5-1646.5 MHz bands are reserved for safety and distress communications.

External links

Notes and References

  1. Web site: ILS PROTON SUCCESSFULLY LAUNCHES INMARSAT-4 F3 SATELLITE . 2008-08-19 . International Launch Services . 2009-02-15 . dead . https://web.archive.org/web/20080923142147/http://www.ilslaunch.com/news-081908 . 2008-09-23 .
  2. Web site: Inmarsat List . US Federal Communications Commission. March 22, 2014. dead. https://web.archive.org/web/20140323091955/http://www.fcc.gov/encyclopedia/inmarsat-list. March 23, 2014.
  3. Web site: Inmarsat-4. Krebs. Gunter. Gunter's Space Page. 2009-02-15.