JCSAT-3A

NORAD 29272· COSPAR 2006-033A· Active satellite· Communications· GEO
Launch
Launched on Aug 11, 2006 from Ariane Launch Area 3, French Guiana aboard a Ariane 5 ECA.
Ariane 5 ECA | JCSAT-10 & Syracuse 3B
Live · TLE epoch 2026-07-13 05:31 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
JAXA
Country
Japan
Manufacturer
Launched
Aug 11, 2006
Mass
Apogee
35,802 km
Perigee
35,785 km
Inclination
0.01°
Period
23.93 h

About JCSAT-3A

JCSAT-3A is a Japanese geostationary communications satellite that has been operating in orbit since August 2006. Catalogued by the United States Space Surveillance Network under NORAD identifier 29272 and internationally designated 2006-033A, the spacecraft occupies a slot in the geostationary belt where it travels in near-perfect synchrony with Earth's rotation. It is operated under the aegis of the SKY Perfect JSAT Group, one of Japan's leading satellite communications providers, and represents a continuation of the long-running JCSAT (Japan Communications Satellite) series that has served Asia-Pacific broadcasting and data communications needs for decades.

Mission and Purpose

JCSAT-3A was developed to extend and reinforce communications infrastructure serving Japan and the broader Asia-Pacific region. The JCSAT series has historically provided capacity for direct-to-home broadcasting, broadband internet access, maritime and aeronautical communications, and enterprise data networking — services that, across a geographically dispersed ocean region dotted with remote islands and archipelagos, are particularly dependent on geostationary relay capacity. Satellite systems of this class fill coverage gaps that terrestrial fiber and microwave networks cannot cost-effectively bridge over open ocean or mountainous terrain.

Before its launch, the spacecraft was referred to internally as JCSAT-10, a working designation common during the development and procurement phase of commercial satellite programs. Upon successful deployment and in-service acceptance, it was redesignated JCSAT-3A, slotting into the operational fleet of SKY Perfect JSAT Group. Although the mission catalog entry maintained by JAXA — the Japan Aerospace Exploration Agency, which holds the operational record as operator — does not publicly detail the specific transponder configuration or service frequencies, communications satellites of this class and era routinely carried Ku-band and sometimes C-band transponder arrays to serve the mix of broadcast and data relay applications typical of commercial operators in this market.

The satellite's mission type and current operational status are not specified in the publicly available tracking catalog, which is not unusual for commercial payloads where detailed service information remains proprietary. What is confirmed is that as of the available catalog data, JCSAT-3A has not undergone a decay or reentry event and remains in orbit.

Orbit and Tracking

JCSAT-3A occupies a position in the geostationary belt, the ring of orbital real estate approximately 35,786 kilometers above Earth's equator where a satellite's orbital velocity matches the planet's rotational rate. At this altitude, a spacecraft appears essentially stationary relative to a ground observer, making it ideal for fixed satellite services such as broadcasting and point-to-point telecommunications links that require persistent, predictable coverage geometry.

The tracked orbital elements for JCSAT-3A reflect a textbook geostationary insertion. Its apogee stands at 35,804 kilometers and its perigee at 35,787 kilometers, giving it an orbit that is nearly perfectly circular, with a difference of only 17 kilometers between its highest and lowest points. Such a tight eccentricity is characteristic of an actively maintained geostationary satellite, where onboard thrusters periodically fire to counteract the gravitational perturbations imposed by the Moon, the Sun, and Earth's own non-uniform mass distribution. The orbital inclination is recorded at 0.0°, meaning the satellite's orbital plane is aligned essentially flush with the equatorial plane — another hallmark of a maintained geostationary asset, since uncontrolled satellites in this belt will gradually develop inclination over time due to lunisolar forces.

The orbital period is 1,436.2 minutes, which corresponds closely to one sidereal day — the time Earth takes to complete one full rotation relative to the stars rather than the Sun. This near-perfect match between orbital period and Earth's rotation rate is precisely what produces the geostationary effect. For ground station operators and end users, this means that dish antennas and uplink facilities can be pointed at a fixed azimuth and elevation without any need for tracking mounts or dynamic pointing corrections, greatly simplifying ground infrastructure.

JCSAT-3A was launched on August 10, 2006. It carries the COSPAR international designator 2006-033A, indicating that it was the first catalogued object from the thirty-third launch of 2006. Tracking data is maintained by the U.S. Space Surveillance Network and made available through public catalogs, allowing satellite enthusiasts, researchers, and operators to monitor its orbital position over time.

Design and Operator

JCSAT-3A was designed and manufactured by Lockheed Martin, the American aerospace and defense company, on the A2100 satellite platform. The A2100 is a well-established commercial satellite bus that Lockheed Martin developed in the 1990s and has deployed on numerous geostationary communications satellites for a variety of international operators. The platform is known for its modular architecture, which allows the payload configuration — the transponders, antennas, and associated electronics — to be adapted across a wide range of mission requirements while the spacecraft bus handles power generation, attitude control, thermal regulation, and propulsion in a standardized way. Satellites built on the A2100 bus have generally demonstrated reliable operational lifespans in the geostationary belt, where commercial operators typically expect fifteen or more years of service from a spacecraft before degraded power or fuel exhaustion ends its useful life.

The spacecraft's specific mass is not recorded in the publicly available tracking catalog. Commercial geostationary satellites of the A2100 class, however, are substantial spacecraft, and launch missions for such payloads typically require heavy-lift launch vehicles with geostationary transfer orbit capability.

The operator of record in the tracking catalog is JAXA, Japan's national space agency, which reflects Japan's role as the satellite's home country and the administrative operator for cataloguing purposes. In practice, SKY Perfect JSAT Group — the commercial entity formed from the merger of JSAT Corporation and SkyPerfecTV — operates the satellite as part of its fleet serving Japan and the surrounding Asia-Pacific region. SKY Perfect JSAT is one of Asia's largest satellite operators and manages a substantial fleet of geostationary spacecraft providing services to broadcasters, telecommunications companies, and government users. JCSAT-3A is among the assets that have contributed to the group's capacity to serve this geographically expansive market.

Current Status and Significance

JCSAT-3A remains in orbit, as confirmed by the absence of any decay or reentry event in its tracking record. Satellites that have exhausted their propellant or reached the end of their commercial service life in the geostationary belt are typically moved to a slightly higher "graveyard orbit" above the operational geostationary arc, where they will remain indefinitely without interfering with active spacecraft. Whether JCSAT-3A is actively transmitting in commercial service, has been placed in a reserve or backup role, or has been retired to a disposal orbit is not specified in the publicly available catalog data.

The spacecraft's continued presence in the geostationary belt underlines a broader characteristic of this orbital regime: geostationary satellites, once placed, do not naturally decay and reenter the atmosphere on any human-relevant timescale. Unlike satellites in low Earth orbit, which experience gradual atmospheric drag and eventually reenter, geostationary objects are effectively permanent fixtures of the near-Earth space environment unless actively deorbited — something the geostationary altitude makes impractical — or relocated to a graveyard disposal orbit. The orbital debris implications of this reality have driven international guidelines encouraging operators to perform end-of-life disposal maneuvers, raising the altitude by a few hundred kilometers to clear the protected geostationary arc.

Within the context of Japan's commercial satellite industry, JCSAT-3A represents one chapter in the evolution of the JCSAT series, which has progressively expanded in capacity and capability since the first JCSAT satellites were deployed in the late 1980s. The series has been instrumental in establishing Japan as a mature and self-sufficient player in the commercial satellite services market, reducing dependence on foreign-owned satellite capacity for domestic broadcasting and telecommunications needs. Satellites like JCSAT-3A have enabled the growth of high-definition broadcasting, VSAT enterprise networks, and broadband connectivity for maritime and aviation customers across one of the world's busiest commercial maritime and aviation corridors.

The A2100 platform's heritage and the sustained presence of JCSAT-3A in catalog records for nearly two decades after launch speaks to the durability of both the spacecraft design and the commercial demand it was built to serve. Though specific operational details are held by SKY Perfect JSAT Group and are not reflected in public tracking data, the satellite's uninterrupted orbital residence since 2006 establishes it as a long-standing element of the geostationary infrastructure that underpins communications across the Asia-Pacific region.

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