ASTRA 3B

NORAD 36581· COSPAR 2010-021A· Active satellite· Communications· GEO
Launch
Launched on May 21, 2010 from Ariane Launch Area 3, French Guiana aboard a Ariane 5 ECA.
Ariane 5 ECA | Astra 3B & COMSATBw-2
Live · TLE epoch 2026-07-13 13:34 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
SES
Country
SES
Manufacturer
Launched
May 21, 2010
Mass
Apogee
35,814 km
Perigee
35,777 km
Inclination
1.54°
Period
23.94 h

About ASTRA 3B

ASTRA 3B is a geostationary communications satellite operated by SES, the Luxembourg-based satellite fleet operator. Launched on May 20, 2010, it occupies the Astra 23.5°E orbital slot and forms part of the broader Astra satellite constellation that has long served as a backbone of European broadcasting and broadband infrastructure. Catalogued by the United States Space Surveillance Network under NORAD ID 36581 and internationally designated 2010-021A, the spacecraft remains in orbit as an active commercial asset delivering a range of broadcast and data services across two continents.

Mission and Purpose

The primary purpose of ASTRA 3B is to provide digital television and radio broadcasting directly to homes and businesses across Europe and into parts of Asia. Operating from the 23.5° East orbital position, the satellite serves as a platform for direct-to-home (DTH) television distribution, enabling broadcasters to reach audiences without the need for intermediate ground-based relay infrastructure. This orbital slot has been developed by SES into a significant broadcast neighborhood, where the concentration of programming carried on co-located satellites encourages consumers to point their dishes toward that position and gain access to a wide variety of channels.

Beyond conventional broadcasting, ASTRA 3B also supports the AstraConnect service, which is SES's two-way satellite broadband offering. This capability allows users in locations underserved by terrestrial internet infrastructure — whether in rural Europe or more remote parts of the coverage zone extending into Asia — to access high-speed internet via a dish-based terminal. Two-way satellite broadband requires the satellite to handle both the forward link (data sent to the user) and the return link (data sent from the user back through the satellite), a more complex capability than simple broadcast distribution. The inclusion of this function in ASTRA 3B's service portfolio reflects the evolution of satellite communications away from one-way broadcast-only platforms toward more interactive, connectivity-oriented services.

The satellite's coverage footprint is designed to serve a geographically broad region. European audiences from the British Isles and Scandinavia in the northwest to southeastern Europe and into Central Asia fall within its service area, making it a genuinely pan-regional asset. This geographic reach aligns with SES's broader commercial strategy of serving both established and emerging broadcast and broadband markets.

Orbit and Tracking

ASTRA 3B operates in geostationary Earth orbit (GEO), the band of orbital space approximately 35,786 kilometers above the equator where a satellite's orbital period matches the rotational period of the Earth. At this altitude, the satellite appears essentially stationary relative to a ground observer, which is a fundamental requirement for the fixed-dish antennas used in DTH broadcasting and broadband services. A dish mounted on a rooftop does not need to track a moving target; it points once at the correct position in the sky and remains there.

The current tracked orbital parameters reflect this geostationary regime closely. ASTRA 3B's apogee is recorded at 35,813 kilometers and its perigee at 35,775 kilometers, giving an orbit that is very nearly circular — the difference between the highest and lowest points is only about 38 kilometers. This near-perfect circularity is characteristic of a well-maintained geostationary spacecraft, as operators routinely perform station-keeping maneuvers to counteract the gravitational perturbations caused by the Moon, the Sun, and the non-uniform mass distribution of the Earth, all of which would otherwise cause the orbit to drift and degrade over time.

The orbital period is 1,436.1 minutes, which is approximately 23 hours and 56 minutes — essentially one sidereal day, confirming synchronization with Earth's rotation. The inclination of 1.5 degrees is a slight deviation from the ideal equatorial plane of a true geostationary orbit. A perfectly maintained geostationary satellite would have an inclination of zero degrees; a small residual inclination like this is common and results either from imprecision in the original orbit injection or from a controlled relaxation of north-south station-keeping, which conserves fuel as the satellite ages but allows the inclination to grow slowly over time. At 1.5 degrees, ASTRA 3B traces a very small figure-eight pattern (known as an analemma) in the sky when viewed from the ground, though this motion is too subtle to affect the alignment of consumer satellite dishes.

The satellite was assigned NORAD catalog number 36581 following its launch and is routinely tracked by the global network of radar and optical sensors that make up the Space Surveillance Network. Its international designator, 2010-021A, encodes its identity as the primary payload of the 21st orbital launch of the year 2010.

Design and Operator

ASTRA 3B was launched on May 20, 2010, entering geostationary transfer orbit before being raised to its operational slot. The satellite is classified as a payload object, distinguishing it from the rocket bodies and debris fragments that are also catalogued from any given launch event. Specific details about the spacecraft's manufacturer and mass are not recorded in the public catalog entry for this object.

The operator, SES, is one of the world's largest satellite fleet operators by revenue and orbital capacity. Headquartered in Betzdorf, Luxembourg, SES manages a large fleet of geostationary and medium-Earth-orbit satellites under both the SES and O3b brand names. The Astra brand specifically refers to the company's geostationary satellites serving the European broadcasting market, a heritage stretching back to the launch of the first Astra satellite in 1988. Over the decades, the Astra constellation has expanded to cover multiple orbital positions, with the fleet at each location carefully coordinated to maximize the number of broadcast channels and services that can be hosted.

SES is registered as both the operator and owner of ASTRA 3B. In the commercial satellite industry, ownership and operational responsibility sometimes reside with different entities — for instance, when a satellite is leased to a third party — but in this case both functions are consolidated within SES. The company generates revenue from this asset primarily by leasing transponder capacity to broadcasters, telecommunications providers, and internet service operators who in turn sell their services to end users.

Current Status and Significance

ASTRA 3B remains in orbit and is not recorded as having decayed or reentered the atmosphere. Its continued operation reflects the typical design lifetime expectations of commercial geostationary communications satellites, which are generally built to operate for fifteen years or more, sustained by onboard propellant reserves used for regular station-keeping.

The satellite's significance within European broadcasting and broadband infrastructure is rooted in the strategic importance of the 23.5°E orbital position. Orbital slots are finite and internationally coordinated resources administered under the framework of the International Telecommunication Union. A well-established neighborhood at a given longitude attracts broadcasters and aggregators because consumers already have dishes aligned to that position, creating a self-reinforcing ecosystem. ASTRA 3B's role at 23.5°E places it within this commercially valuable context.

The provision of two-way broadband through the AstraConnect service also positions the satellite within a longer-term trend in European communications policy. Successive European Union frameworks have identified universal broadband access as a policy objective, and satellite connectivity has been recognized as a key tool for reaching rural and remote populations for whom terrestrial fixed-line or mobile broadband is economically or technically impractical. Satellites operating at geostationary altitude have inherent latency constraints — the roughly 35,800-kilometer round trip for a signal introduces a delay of approximately half a second — but for many applications this remains an acceptable trade-off for coverage availability.

From a historical standpoint, ASTRA 3B was launched at a point when the satellite broadcasting industry was navigating the transition from standard-definition to high-definition television, as well as early interest in 3D broadcasting. The additional capacity brought online by the satellite at its orbital position contributed to the bandwidth available for higher-quality broadcast formats across the European market.

As a geostationary object at roughly 35,000 kilometers altitude, ASTRA 3B is far beyond the reaches of low Earth orbit and poses no collision risk to crewed spaceflight infrastructure or the dense population of satellites in LEO. At end of life, geostationary satellites are conventionally raised into a "graveyard" orbit several hundred kilometers above the geostationary belt, clearing the operationally valuable slot for successors. Whether ASTRA 3B has reached or is approaching that phase is not reflected in the current catalog data, which continues to record the satellite as present in its operational orbital regime.

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