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Inmarsat-4 F3
| Field | Value |
|---|---|
| name | Inmarsat-4 F3 |
| operator | Inmarsat |
| spacecraft_bus | Eurostar E3000 |
| manufacturer | EADS Astrium |
| launch_mass | 5960 kg |
| launch_date | |
| launch_rocket | Proton-M/Briz-M |
| launch_site | Baikonur 200/39 |
| launch_contractor | ILS |
| entered_service | 7 January 2009 |
| deactivated | |
| 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, by a Proton-M/Briz-M Enhanced carrier rocket. It is currently located at 97.65° West longitude, providing coverage of the Americas. 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. 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.
References
References
- (2008-08-19). "ILS PROTON SUCCESSFULLY LAUNCHES INMARSAT-4 F3 SATELLITE". International Launch Services.
- "Inmarsat List".
- Krebs, Gunter. "Inmarsat-4". Gunter's Space Page.
This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.
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