Official name ALPHASAT (I-4A F4)
Alternative name Alphasat
Cospar ID 2013-038A
Norad ID 39215
Launch date 2013-07-25
Launch site FRGUI
Launch vehicle Ariane-5ECA
Country/Organization International
Type application Communication
Operator ESA, Inmarsat
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.19
Inclination (deg) 2.89
Perigee (km) 35777
Apogee (km) 35800
Eccentricity 0.00032133227153974
Mean motion (revs. per day) 1.00265285233848
Semi-Major axis (km) 42166.635
Raan (deg) 7.851
Arg of perigee (deg) 75.4171
Shape Box + 2 Pan + 1 Dish
Mass (kg) 6650
Height (m) 7.1
Width (m) 2.5
Depth (m) 2.5
Span (m^2) 40
Lifetime 15 years
Contractors EADS Astrium, Thales Alenia Space
Equipment L-band payload
Propulsion EAM, PPS-1350-G plasma thrusters
Configuration Alphabus
Power 2 deployable solar arrays, batteries

Alphasat or Inmarsat-4A F4 (originally Alphasat I-XL or Inmarsat XL) is a joint ESA and Inmarsat communications satellite using the Alphabus proto-flight platform, achieving in-orbit validation of the ESA initiated platform through a commercial operator.

Alphasat features a new generation digital signal processor for the payload, and a 12-meter aperture antenna reflector. The spacecraft has a mass of 6649 kg at launch, an electrical power of 12 kW. Planned for launch in 2012, Alphasat has a design lifetime of 15 years.

Inmarsat flew an extended L-band payload, in parallel to and supporting its existing world-leading global mobile satellite services. This Inmarsat mission definition is based around multimedia mobile services already provided by the current Inmarsat-4 satellites through Broadband Global Area Network (GAN)

The satellite is positioned at 25 degrees east, with its coverage centred over Africa and providing additional coverage to Europe, the Middle-East and parts of Asia.

Implementation of this Geo-mobile application uses the Alphabus platform design in a configuration that requires a 90 degree change to the satellite flight orientation to improve accommodation of the feed/reflector configuration and allow the embarkation of a large deployable reflector. Both of these capabilities are offered as options in the Alphabus portfolio.

In addition, Alphasat embarks three ESA-provided technology demonstration payloads:

  • An advanced laser communication terminal to demonstrate LEO to GEO communication links at 2 Gbit/s,
  • Two Q/V-band communication experiments to assess the feasibility of these bands for future commercial applications,
  • An advanced startracker with active pixel detector,
  • An environment effects facility to monitor the GEO radiation environment and its effects on electronic components and sensors.

The Alphasat programme meets the diverse but mutually compatible goals of all the parties, such as the first flight and in-orbit verification of Alphabus and the implementation of an advanced L-band operational payload, which supplements the existing Inmarsat satellite constellation and offer the opportunity for new and advanced services.

The contract was signed in November 2007 with a launch targeted by 2013.

Satellite COSPAR Date LS Launch Vehicle Remarks
ALPHASAT (I-4A F4) 2013-038A 2013-07-25 FRGUI Ariane-5ECA with Insat 3D