Samiksha Jaiswal (Editor)

Inmarsat 4A F4

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
COSPAR ID
  
2013-038A

Mission duration
  
15 years

Inclination
  
0.14°

Launch mass
  
6,649 kg

Bus
  
SATCAT no.
  
39215

Inclination
  
0.14°

Period
  
24 hours

Launch date
  
25 July 2013

Inmarsat-4A F4 Alphasat Inmarsat Satellite Missions eoPortal Directory

Mission type
  
CommunicationsTechnology

Operator
  
InmarsatEuropean Space Agency

Manufacturer
  
EADS AstriumThales Alenia Space

Similar
  
INSAT‑3D, Sentinel‑1A, SES‑6, HYLAS‑1, Artemis

Inmarsat-4A F4, also known as Alphasat and Inmarsat-XL, is a large geostationary communications I-4 satellite operated by UK based Inmarsat in partnership with the European Space Agency. Launched in 2013, it is used to provide mobile communications to Africa and parts of Europe and Asia.

Inmarsat-4A F4 Inmarsat Coverage SatPhoneCity

Inmarsat-4A F4 has been constructed by EADS Astrium and Thales Alenia Space based on the Alphabus satellite bus. It was the first Alphabus spacecraft to be launched, and as such it carries several experimental communications systems in addition to its commercial payload. The spacecraft had a launch mass of 6,649 kilograms (14,659 lb), and is expected to operate for at least fifteen years.

Inmarsat-4A F4 httpsuploadwikimediaorgwikipediacommonsthu

Arianespace had been contracted to launch Inmarsat-4A F4, with an Ariane 5ECA rocket, flight number VA-214, delivering it and INSAT-3D into geosynchronous transfer orbit. The rocket lifted off from ELA-3 at Kourou at 19:54:07 UTC on 25 July 2013, with Inmarsat-4A F4 separating from the rocket around 27 minutes later.

Inmarsat-4A F4 Alphasat Inmarsat4A F4 Gunter39s Space Page

The spacecraft operates in a geostationary orbit at a longitude of 25 degrees east. As of 29 October 2013, it is in an orbit with a perigee of 35,771 kilometres (22,227 mi), an apogee of 35,771 kilometres (22,227 mi) and 0.14 degrees inclination to the equator. The orbit had a semimajor axis of 42,157.20 kilometres (26,195.27 mi) and eccentricity of 0.0003552, giving it an orbital period of 1,435.75 minutes, or 23.92 hours.

Inmarsat-4A F4 Alphasat Technology demonstration YouTube

European Data Relay System test

Inmarsat-4A F4 Alphasat Inmarsat Satellite Missions eoPortal Directory

The satellite was used as part of a in-orbit verification of the ESA European Data Relay System. In 2014, data from the Sentinel-1A satellite in LEO was transmitted via an optical link to the Alphasat in GEO and then relayed to a ground station using a Ka band downlink. The new system can offer speeds up to 7.2 Gbit/s in the future.

References

Inmarsat-4A F4 Wikipedia