ASIASTAR

NORAD 26107· COSPAR 2000-016A· Active satellite· Communications· GEO
Launch
Launched on Mar 21, 2000 from Ariane Launch Area 3, French Guiana aboard a Ariane 5 G.
Ariane 5 G | INSAT-3B & AsiaStar
Live · TLE epoch 2026-07-13 13:57 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
1worldspace
Country
United States
Manufacturer
Launched
Mar 21, 2000
Mass
Apogee
35,810 km
Perigee
35,779 km
Inclination
9.19°
Period
23.94 h

About ASIASTAR

ASIASTAR (also cataloged under the designation AsiaStar) is an American communications satellite that was placed into geostationary orbit in March 2000. Operated by the satellite radio and data broadcasting company 1worldspace, the spacecraft was designed to deliver digital audio broadcasting and multimedia services across Asia. It remains one of the more notable examples of late-1990s commercial satellite expansion into the Asian communications market, a period defined by ambitious plans to bring subscription-based audio broadcasting to underserved populations across an enormous geographic footprint. ASIASTAR carries the NORAD catalog identifier 26107 and the international COSPAR designator 2000-016A.

Mission and Purpose

ASIASTAR was developed as part of 1worldspace's broader ambition to replicate a subscription-based digital audio broadcasting model across multiple continents simultaneously. The company, which also operated satellites serving Africa and parts of the Middle East through its AfriStar platform, envisioned a world in which listeners in rural or remote regions — places where terrestrial radio infrastructure was sparse or unreliable — could receive high-quality digital audio content via compact, affordable receivers. For the Asian market, ASIASTAR was the cornerstone of that plan.

The satellite's coverage was intended to span a substantial portion of the Asia-Pacific region, reaching populations across South Asia, Southeast Asia, and parts of Central and East Asia. The 1worldspace model relied on direct-to-listener broadcasting in the S-band frequency range, with subscribers using purpose-built receivers to access programming. The service model represented a significant departure from conventional terrestrial radio, positioning satellite-delivered content not merely as a luxury but as a practical solution for regions where broadcast infrastructure lagged far behind population needs.

While the mission concept was compelling, 1worldspace ultimately struggled commercially. The company filed for bankruptcy protection in 2008, and its operational footprint contracted significantly in the years that followed. The precise current operational status of ASIASTAR is not publicly confirmed in available catalog records, and whether the satellite continues to provide any active services is not definitively established. What is clear is that the spacecraft remains in orbit as of the time of writing.

Orbit and Tracking

ASIASTAR occupies a geostationary orbit, the class of orbit located approximately 35,786 kilometers above the equator in which a satellite's orbital period matches the Earth's rotation, causing it to appear stationary relative to a fixed point on the ground. This orbit class is the standard choice for telecommunications and broadcasting satellites, as it allows a single spacecraft to maintain continuous coverage of a large geographic region without the need for a ground-based tracking infrastructure to follow its movement across the sky.

The verified orbital parameters for ASIASTAR reflect its geostationary positioning with precision. Its apogee stands at 35,816 kilometers and its perigee at 35,773 kilometers, indicating a near-circular orbit with a difference of only 43 kilometers between its highest and lowest points — characteristic of a well-maintained geostationary slot. The orbital period is recorded at 1,436.1 minutes, which corresponds closely to one sidereal day and confirms the satellite's synchronization with Earth's rotation.

One notable element of ASIASTAR's orbital profile is its inclination of 9.1 degrees relative to the equatorial plane. A perfectly maintained geostationary satellite would ideally hold an inclination of zero degrees, remaining fixed directly above the equator. An inclination of 9.1 degrees suggests that the satellite has been allowed to drift into what is commonly termed a "graveyard" or passively maintained configuration, where north-south station-keeping maneuvers — which require fuel — are no longer being performed. Under these conditions, the satellite traces a slow figure-eight pattern, known as an analemma, over its nominal equatorial position as seen from the ground. This is a well-understood phenomenon and is generally consistent with a spacecraft that has either exhausted its station-keeping fuel reserves or for which active operational maintenance is no longer economically justified.

ASIASTAR can be tracked using its NORAD ID 26107, and its current orbital elements are updated regularly in public satellite databases.

Design and Operator

ASIASTAR was built through a collaboration between Matra Marconi Space and Alcatel Space, two prominent European aerospace firms that were, at the time of the satellite's construction, among the leading manufacturers of commercial communications spacecraft on the continent. The satellite was based on the Eurostar E2000+ bus, a platform developed by what was then Matra Marconi Space and widely used for a generation of commercial geostationary satellites during the 1990s and early 2000s. The E2000+ bus offered a well-proven foundation for high-power telecommunications payloads, with a design heritage that made it a competitive choice for operators seeking reliability in geostationary applications. The satellite's mass is not confirmed in public catalog records.

The launch of ASIASTAR took place on 21 March 2000, at 23:29 UTC, making the nominal launch date — accounting for time zones — the evening of 20 March 2000 in North American Eastern Standard Time. The launch was conducted by Arianespace, the French-led commercial launch consortium that has operated from the Centre Spatial Guyanais in Kourou, French Guiana, since the early 1980s. The vehicle used was an Ariane 5G, the initial operational variant of the Ariane 5 rocket family, flying from the ELA-3 launch complex at the Guiana Space Centre. Ariane 5, at that point still relatively early in its commercial operational career following its troubled debut in 1996, had established itself as a capable heavy-lift launcher for dual-payload geostationary missions.

ASIASTAR shared its ride to orbit with INSAT-3B, an Indian multipurpose communications satellite operated by the Indian Space Research Organisation. Dual-payload launches on Ariane 5 were a standard commercial practice of the era, allowing Arianespace to maximize the revenue potential of each mission and reduce per-kilogram launch costs for satellite operators by splitting the price of a launch between two customers.

The operator, 1worldspace, was incorporated in the United States and headquartered in Washington, D.C. The company was founded by Noah Samara and pursued an idealistic as well as commercial vision of democratizing access to information through satellite broadcasting. Despite significant investment and genuine technological ambition, the business model proved difficult to sustain at scale, and the company's financial difficulties eventually overshadowed its operational achievements.

Legacy and Current Status

ASIASTAR occupies a complex place in the history of commercial satellite communications. It was a technically accomplished spacecraft, built on a reputable European platform, deployed by one of the world's leading launch providers, and conceived with a genuine social purpose: broadening access to information and entertainment across Asia's vast and diverse landscape. The 1worldspace concept predated the widespread availability of internet-based audio streaming and represented an early, serious attempt to solve the problem of information access in low-infrastructure regions through space-based technology.

The company's collapse in 2008 — followed by restructuring attempts that never fully restored its original ambitions — left ASIASTAR in an ambiguous position. The satellite itself, built to last in the harsh environment of geostationary orbit, outlasted the commercial enterprise that launched it. Its current inclination of 9.1 degrees, significantly above the near-zero values associated with actively maintained geostationary satellites, is consistent with a spacecraft in a passively drifting state. This does not necessarily mean the satellite is entirely non-functional, but it strongly suggests that regular north-south station-keeping is no longer being conducted.

In the broader context of geostationary satellite history, ASIASTAR represents a generation of commercially operated broadcasting satellites that sought to leapfrog terrestrial infrastructure in the developing world — a goal that has since been pursued through many different technological approaches, from low-cost mobile data to small satellite constellations. The 1worldspace model did not ultimately prevail, but it contributed to the global conversation about how satellite technology could serve populations beyond the reach of conventional broadcast and telecommunications networks.

For satellite observers and historians, ASIASTAR remains a trackable object in the geostationary belt. Its NORAD catalog ID of 26107 and COSPAR designator 2000-016A allow its position and orbital evolution to be followed through public space surveillance databases. As a geostationary object at roughly 35,800 kilometers altitude, it presents no reentry risk in any near-term timeframe and is expected to remain in the high-altitude graveyard belt for the foreseeable future — a durable artifact of an ambitious chapter in commercial satellite history.

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