AMC-6

NORAD 26580· COSPAR 2000-067A· Active satellite· Communications· GEO
Launch
Launched on Oct 21, 2000 from 81/23 (81L), Kazakhstan aboard a Proton-K/DM-2M.
Proton-K/DM-2M | GE 6
Live · TLE epoch 2026-07-13 14:31 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
SES Americom
Country
SES
Manufacturer
Launched
Oct 21, 2000
Mass
Apogee
35,811 km
Perigee
35,779 km
Inclination
0.22°
Period
23.94 h

About AMC-6

AMC-6 is a commercial geostationary communications satellite operated by SES Americom. Assigned NORAD catalog ID 26580 and international designator 2000-067A, it was launched on October 20, 2000, from the Baikonur Cosmodrome in Kazakhstan. Originally designated GE-6 at the time of its launch, the satellite was subsequently renamed AMC-6 following a corporate reorganization that brought it under the SES Americom brand. As of the time of writing, the spacecraft remains in orbit and continues to occupy a geostationary position above the Americas.

Mission and Purpose

AMC-6 was designed to serve as a commercial broadcast and telecommunications relay satellite, providing coverage across an extensive geographic footprint that encompasses the continental United States, Canada, the Caribbean, southern Greenland, and portions of Latin America. This broad arc of coverage made it a natural choice for operators requiring reliable connectivity across widely dispersed ground terminals, including both commercial enterprises and government users.

Among the satellite's primary service capabilities is support for Very-Small-Aperture Terminal (VSAT) networking — a technology that allows geographically distributed locations, such as retail outlets, branch offices, or remote government sites, to connect via compact dish antennas without relying on terrestrial infrastructure. VSAT services have long been a cornerstone of satellite communications for enterprises that need wide-area private networks at relatively low ground-equipment cost, and AMC-6's broad beam geometry made it well suited for this application.

The satellite also supports satellite news gathering (SNG) operations, a mission type that demands reliable, high-bandwidth uplink capability at short notice and often from portable or rapidly deployed terminals. News organizations and broadcasters covering events across North America and the wider Western Hemisphere have historically drawn on C-band and Ku-band capacity from satellites positioned along the arc that AMC-6 occupies, and the satellite's hybrid C-band/Ku-band architecture made it especially flexible for such varied broadcast requirements.

In addition to broadcast and VSAT services, AMC-6 has been used as a platform for Internet delivery. Geostationary satellites positioned over wide population centers can serve as effective internet distribution nodes, particularly for thinly served or rural areas where terrestrial broadband is limited. The satellite's geographic reach and redundancy characteristics supported this role, making it a platform of interest not only for narrowcast business applications but also for broader consumer-facing connectivity services.

The specific mission status and current service configuration of AMC-6 are not publicly detailed in the satellite catalog, and no confirmed operational details beyond these established service types are available in open records.

Orbit and Tracking

AMC-6 operates in a geostationary orbit, the class of orbit in which a satellite travels at an altitude and speed that allows it to remain effectively stationary relative to a fixed point on Earth's surface. This makes geostationary satellites ideal for communications applications, since ground antennas can be aimed at a fixed point in the sky without requiring tracking mounts.

According to current orbital data, AMC-6 has an apogee of 35,811 km and a perigee of 35,778 km, indicating a very nearly circular orbit at the canonical geostationary altitude of approximately 35,786 km above the equator. The slight difference between apogee and perigee represents a minimal eccentricity consistent with normal station-keeping operations. The satellite's orbital inclination is 0.1°, essentially equatorial, which is consistent with the requirements of geostationary operation. An inclination of exactly zero degrees is the theoretical ideal for a geostationary satellite, and the 0.1° figure reflects the practical reality that even well-maintained geostationary satellites are subject to minor perturbations from gravitational influences, including the oblateness of the Earth and the gravitational effects of the Moon and Sun.

The orbital period is recorded as 1,436.1 minutes — almost precisely 23 hours and 56 minutes, which is the length of a sidereal day. This synchronization between the satellite's orbital period and Earth's rotation rate is what produces the geostationary effect, keeping the spacecraft parked over a nearly fixed longitude as seen from the ground.

AMC-6 is positioned along the geostationary arc in a location broadly corresponding to the eastern portion of the Americas, a slot that gives it the wide-area line of sight it needs to serve its stated coverage zones. Because geostationary satellites sit at such great altitude, they are not typically observed by casual stargazers under normal circumstances. At their operating distance, even large spacecraft appear as extremely faint, slow-moving or stationary points, and are generally only detectable with optical aid under the right conditions.

Design and Operator

AMC-6 was built as a hybrid satellite carrying both C-band and Ku-band transponder payloads. This dual-band architecture reflects a deliberate design philosophy: C-band frequencies offer greater resilience in adverse weather conditions, including heavy rainfall, while Ku-band transponders support higher-frequency applications, including direct broadcast and high-throughput data services. The combination made AMC-6 a versatile platform capable of serving a wide range of customers with differing technical requirements.

The manufacturer of AMC-6 is not recorded in publicly available catalog data. The satellite's mass at launch is similarly not available in the current catalog entry.

At the time of its launch in 2000, the satellite was operated under the GE Americom banner, reflecting GE Capital's then-ownership of the Americom satellite fleet. GE-6, as it was then known, represented the fifth satellite in GE Americom's hybrid C-band/Ku-band series — a family of spacecraft designed to meet the growing demand for flexible, multi-service geostationary capacity over the Americas in the late 1990s and early 2000s.

The corporate landscape changed significantly in 2001 when Luxembourg-based SES acquired GE Americom, creating the entity known as SES Americom. As part of this transition, the GE-branded satellite fleet was renamed under the AMC designation, and GE-6 became AMC-6. SES subsequently continued to reorganize its North American and global satellite assets, and SES Americom was eventually merged with SES New Skies in 2009, forming SES World Skies. The satellite's operator is recorded in current databases as SES Americom, reflecting this lineage, and the owner country is listed as SES — referring to the Luxembourg-based parent company rather than a nation-state per se.

Legacy and Current Status

AMC-6 launched into a period of significant growth and transformation in the commercial satellite communications industry. The late 1990s and early 2000s saw rapid expansion in demand for broadband Internet access, satellite television, and enterprise networking, all of which drove demand for the kind of flexible, wide-coverage geostationary capacity that AMC-6 was designed to provide. As one of the fifth-generation hybrid satellites in the GE Americom fleet, it was well positioned to serve the evolving needs of that market.

The renaming from GE-6 to AMC-6 was part of a broader rebranding effort that accompanied SES's expansion into the North American market. The transition was representative of broader consolidation trends in the satellite industry during the early 2000s, as major European and global operators acquired North American fleets to achieve economies of scale and broader geographic reach.

As of the date of this entry, AMC-6 remains in orbit. Current orbital elements indicate it continues to occupy a near-equatorial geostationary position with the orbital characteristics described above — an apogee of 35,811 km, a perigee of 35,778 km, an inclination of 0.1°, and a period of 1,436.1 minutes. No decay or reentry date has been recorded, consistent with the long operational and graveyard-orbit lifespans typical of geostationary communications satellites. When a geostationary satellite reaches the end of its operational life, standard practice in the industry calls for it to be raised into a slightly higher "graveyard" orbit, safely above the geostationary belt, to free up the orbital slot for successor spacecraft. Whether AMC-6 is currently operational, in a reduced-service configuration, or has been retired to such a graveyard orbit is not confirmed in publicly available catalog records.

AMC-6 represents a snapshot of the transitional era in commercial satellite communications — a period when C/Ku hybrid platforms were becoming standard, when broadband Internet via satellite was emerging as a serious commercial proposition, and when the industry was consolidating from a fragmented landscape of national and corporate operators into a smaller number of large global fleets. Its two decades and more in orbit place it among the longer-running artifacts of that pivotal era in orbital infrastructure.

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