ALPHASAT

NORAD 39215· COSPAR 2013-038A· Active satellite· Communications· GEO
Launch
Launched on Jul 25, 2013 from Ariane Launch Area 3, French Guiana aboard a Ariane 5 ECA.
Ariane 5 ECA | Alphasat I-XL (Inmarsat-XL) & INSAT-3D
ALPHASAT
Yves Chassang, donne autorisation par mail à Guy Lebègue pour publication selon licence Creative Commons correcte · CC BY-SA 3.0 · via Wikimedia Commons
Live · TLE epoch 2026-07-12 22:11 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
European Space Agency
Country
Inmarsat
Manufacturer
Thales Alenia Space
Launched
Jul 25, 2013
Mass
6,649 kg
Apogee
35,804 km
Perigee
35,785 km
Inclination
3.00°
Period
23.94 h

About ALPHASAT

ALPHASAT (also cataloged under the international designator 2013-038A and NORAD ID 39215) is a large geostationary communications satellite operated jointly by the UK-based satellite services company Inmarsat and the European Space Agency (ESA). Also known by the designations Inmarsat-4A F4 and Inmarsat-XL, it was launched on July 24, 2013, and remains operational in geostationary orbit today. At launch it weighed approximately 6,649 kilograms, making it one of the heaviest commercial communications satellites placed into orbit at the time of its deployment. The spacecraft was built by Thales Alenia Space and serves as both a commercial telecommunications asset and a technology demonstration platform of considerable importance to European space development.

Mission and Purpose

ALPHASAT was conceived as a dual-purpose spacecraft, combining a commercial mobile satellite communications role with a significant technology validation mission undertaken in partnership with ESA. On the commercial side, the satellite extended and enhanced Inmarsat's global mobile communications network, with its coverage footprint directed primarily at Africa, alongside portions of Europe and Asia. This regional emphasis addressed growing demand for reliable broadband and voice connectivity in areas where terrestrial infrastructure remains limited or uneven, including maritime and aeronautical users operating across the African continent and surrounding waters.

The ESA partnership dimension of ALPHASAT is a defining feature of the program. Under ESA's Advanced Research in Telecommunications Systems (ARTES) program, the agency co-funded the satellite's development as a vehicle for testing new European space technologies in the harsh environment of geostationary orbit. Several hosted payloads — small experimental packages from European research institutions and companies — were integrated into the spacecraft alongside the primary communications payload. These technology demonstration experiments covered areas including optical inter-satellite link demonstrations, navigation signal monitoring, and new radio-frequency technologies, providing in-orbit validation that would be difficult or impossible to replicate in ground testing alone. This blending of commercial operations with ESA research objectives represents a model of public-private cooperation that the agency has sought to expand.

The satellite joined Inmarsat's constellation of I-4 series spacecraft, a family of high-capacity mobile broadband platforms providing L-band services globally. While the specific operational parameters and current service status are not publicly recorded in the satellite catalog, the I-4 architecture has historically supported maritime, aeronautical, land-mobile, and government users requiring reliable connectivity independent of ground-based networks.

Orbit and Tracking

ALPHASAT occupies a geostationary orbit, a regime roughly 35,786 kilometers above the equator at which a satellite's orbital period matches Earth's rotation and the spacecraft appears to hover at a fixed point in the sky as viewed from the ground. The satellite's current tracked orbital parameters reflect this placement precisely: its apogee stands at 35,803 kilometers and its perigee at 35,787 kilometers, indicating an almost perfectly circular orbit with minimal eccentricity. The orbital period is 1,436.2 minutes — very close to one sidereal day — confirming that the spacecraft is well-positioned within the geostationary belt.

The inclination of 3.0 degrees is a modest but notable departure from a perfectly equatorial orbit. A true, station-kept geostationary satellite operates at or near zero inclination, causing it to trace a small figure-eight pattern (known as an analemma) in the sky rather than remaining at an absolutely fixed point. An inclination of 3.0 degrees is within the range that suggests either some ongoing natural drift away from a zero-inclination station, or that active north-south stationkeeping has been relaxed or reduced to conserve propellant — a common practice as a satellite ages, extending operational life by allowing inclination to drift while continuing to provide service. Whether this reflects the satellite's normal operational posture or a phase in its extended mission cannot be determined from catalog data alone.

Because ALPHASAT is in geostationary orbit, tracking it requires somewhat different methods than tracking low Earth orbit satellites. It does not pass overhead in the manner of lower objects; instead, observers at fixed ground stations in Europe, Africa, or Asia can point a dish or antenna toward a consistent bearing in the sky and maintain a link without continuous repointing. For space-tracking purposes, its position is updated regularly in orbital element catalogs, and it can be identified by its NORAD catalog number 39215 or by its international designator 2013-038A in databases such as the one maintained by the US Space Surveillance Network.

Design and Operators

ALPHASAT was designed and manufactured by Thales Alenia Space, a Franco-Italian aerospace manufacturer with deep experience in large geostationary telecommunications platforms. The spacecraft's launch mass of 6,649 kilograms placed it among the heaviest commercial satellites of its generation, a reflection of its large communications payload, the hosted technology demonstration payloads, and the propellant required for a long operational life in geostationary orbit. Satellites of this class are typically designed for operational lifetimes of fifteen years or more, sustained by onboard propulsion systems used to correct orbital perturbations and maintain the correct orbital slot.

Inmarsat, the satellite's owner, is a British company with a long history in mobile satellite services stretching back to its origins as an international intergovernmental organization in the late 1970s. Now a private commercial entity, Inmarsat operates a global fleet of geostationary and, more recently, low Earth orbit satellites, providing connectivity services to customers across the maritime, aviation, government, and enterprise sectors.

ESA's involvement as co-operator reflects the agency's strategic interest in developing European capabilities in satellite communications technology. By partnering with a commercial operator to fly experimental payloads on an operational spacecraft, ESA was able to reduce the cost and risk of technology demonstration while ensuring that European researchers and industry gained access to real in-orbit test conditions. This kind of co-funded, multi-purpose satellite model has influenced subsequent ESA ARTES initiatives and is considered a meaningful contribution to the European space industry's competitiveness.

Significance and Legacy

ALPHASAT holds a notable place in European commercial space history primarily because of its scale and the breadth of its mission objectives. At the time of its launch in mid-2013, it represented one of the largest and most capable commercial telecommunications satellites built by a European manufacturer, serving as a demonstration that Thales Alenia Space and the broader European space industrial base could compete at the forefront of high-mass geostationary satellite construction.

The satellite's dual commercial and research role became something of a template for how ESA and industry partners could co-invest in space infrastructure to mutual benefit. Rather than flying a dedicated, purely governmental research satellite at high cost, ESA leveraged Inmarsat's commercial launch and operations to place multiple technology experiments in orbit for a fraction of what standalone missions would have required. The hosted payload approach demonstrated aboard ALPHASAT has since appeared in ESA planning documents as a viable pathway for validating future technologies — from optical communications to new navigation payloads — in the demanding environment of deep space.

From a communications perspective, ALPHASAT extended L-band mobile coverage into regions of Africa that had previously been underserved by satellite capacity, contributing to maritime safety communications, humanitarian logistics, and governmental connectivity across a continent where reliable communications infrastructure remains an ongoing challenge. While specific current service metrics are not documented in publicly available catalogs, the satellite's continued presence in orbit more than a decade after launch indicates that it has delivered operational value well beyond any minimum mission threshold.

The satellite's longevity also serves as a practical test bed. Technology demonstration payloads aboard ALPHASAT have operated in the radiation environment of geostationary orbit for an extended period, yielding data about component performance and degradation that ground simulations cannot replicate with full fidelity. This in-orbit heritage information feeds back into the design of future European spacecraft, making ALPHASAT a contributor to European space competence in ways that extend beyond its direct communications services.

For observers and researchers using this catalog, ALPHASAT represents a class of large, operationally significant geostationary assets that are tracked not because they pass across the sky in visible arcs, but because their stable orbital positions and known parameters allow ground systems — from professional antenna arrays to research receivers — to locate and monitor them with confidence. Its record in the catalog, anchored by NORAD ID 39215 and international designator 2013-038A, ensures that it remains unambiguously identifiable in the global space surveillance network for as long as it remains in orbit.

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