JCSAT-5A

NORAD 29045· COSPAR 2006-010A· Active satellite· Communications· GEO
Launch
Launched on Apr 12, 2006 from Launch Platform Odyssey aboard a Zenit 3SL.
Zenit | JCSAT 5A
Live · TLE epoch 2026-07-13 12:22 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
SKY Perfect JSAT Holdings
Country
Japan
Manufacturer
Launched
Apr 12, 2006
Mass
Apogee
35,802 km
Perigee
35,788 km
Inclination
1.18°
Period
23.94 h

About JCSAT-5A

JCSAT-5A is a Japanese geostationary communications satellite operated by SKY Perfect JSAT Holdings, one of Japan's largest satellite communications providers. Assigned the NORAD catalog identifier 29045 and the international designator 2006-010A, the spacecraft was launched on April 12, 2006 (April 11 in US Eastern time), and remains in service in geostationary orbit as of the time of writing. The satellite is also designated N-STAR d, reflecting its dual role within both the JCSAT commercial network and the N-STAR system operated in cooperation with NTT. Prior to its launch, the spacecraft was referred to internally as JCSAT-9.

Mission and Purpose

JCSAT-5A was developed to extend and reinforce the communications infrastructure that SKY Perfect JSAT operates across the Asia-Pacific region. The JCSAT network has long served as a backbone for direct-to-home broadcasting, broadband data services, and business communications spanning Japan and neighboring territories. By augmenting the existing fleet with an additional geostationary asset, the operator was able to increase capacity and provide redundancy in a region with substantial demand for satellite-delivered content and connectivity.

The N-STAR designation connects the satellite to a distinct but complementary lineage. The N-STAR series was originally conceived as a cooperative program to serve domestic Japanese telecommunications requirements, including government and public-sector applications. By bearing both the JCSAT-5A and N-STAR d identities, the satellite bridges the commercial and institutional dimensions of Japan's satellite communications ecosystem. This kind of dual-identity arrangement is not unusual in the Japanese market, where consolidation among satellite operators has often resulted in legacy naming conventions being carried forward even as fleets are restructured and responsibilities are reorganized.

The specific payload configuration and transponder complement of JCSAT-5A are not recorded in the public tracking catalog. However, satellites of its class and era typically carry Ku-band and, in some configurations, Ka-band or C-band transponders tailored to regional coverage footprints. Given the satellite's operational context — serving Japanese and broader Asia-Pacific audiences — its communications payload would logically have been optimized for those markets. The mission status and current operational condition are not confirmed in publicly available catalog records, which means definitive statements about whether the spacecraft remains in active commercial service cannot be made with certainty on the basis of verified data alone.

Orbit and Tracking

JCSAT-5A occupies a geostationary orbit, the class of orbit situated approximately 35,786 kilometers above the Earth's equator where a satellite's orbital period matches the planet's rotation, causing the spacecraft to appear essentially stationary from the ground. This characteristic makes geostationary slots exceptionally valuable for communications applications, since ground antennas can be fixed rather than requiring active tracking mechanisms.

Current orbital elements place JCSAT-5A at an apogee of 35,804 kilometers and a perigee of 35,787 kilometers, figures that reflect the slight ellipticity inherent even in operationally geostationary spacecraft. The orbital inclination is measured at 1.1 degrees, a small but nonzero deviation from the ideal equatorial plane. For satellites that are still being actively controlled by their operators, inclination is typically maintained very close to zero through periodic north-south stationkeeping maneuvers. An inclination of 1.1 degrees may suggest that such stationkeeping efforts have been reduced or suspended, which sometimes occurs as a satellite ages and its propellant reserves diminish, or if the spacecraft has been transitioned to a more passive operational posture. However, this interpretation should be treated with appropriate caution, as inclination can vary for other operational reasons as well.

The orbital period of JCSAT-5A is 1,436.2 minutes, very close to the 1,436-minute period associated with a true geostationary orbit synchronized to one sidereal day. The slight departure from a perfectly circular, equatorial path means that observers on the ground would see the satellite trace a small figure-eight pattern — known as an analemma — rather than remaining at a perfectly fixed point in the sky. This drift is typically imperceptible to casual observers but is relevant for precision antenna pointing in professional installations.

The satellite was cataloged under COSPAR designator 2006-010A, identifying it as the primary payload of the tenth launch of 2006 as recorded in the international space object registry. It has remained in orbit continuously since that launch and has not experienced a decay or reentry event.

Design and Operator

JCSAT-5A was built on the Lockheed Martin A2100 satellite platform, a widely used spacecraft bus that has underpinned dozens of commercial communications satellites since its introduction in the 1990s. The A2100 is known for its modular design, which allows the bus to be configured across a broad range of mission sizes and payload requirements. The platform has been selected by numerous operators worldwide for its reliability and the heritage accumulated across an extensive flight history. The manufacturer of JCSAT-5A, as listed in the tracking catalog, is not publicly confirmed, though the background context establishes Lockheed Martin's role in the spacecraft's development.

The operator, SKY Perfect JSAT Holdings, is the product of a merger between Japan Satellite Systems (JSAT) and SkyPerfecTV, consolidating much of Japan's commercial satellite capacity under a single corporate umbrella. The company operates one of the largest fleets of communications satellites serving the Asia-Pacific region, and JCSAT-5A represents one element of that broader infrastructure investment. SKY Perfect JSAT is headquartered in Japan, reflecting the satellite's national origin as documented in the tracking registry.

The mass of JCSAT-5A is not recorded in the public catalog data available to this database. While the A2100 platform can accommodate spacecraft across a considerable range of launch masses depending on configuration, any specific figure for this satellite would be speculative without authoritative source confirmation.

Current Status and Significance

JCSAT-5A holds a place in the history of Japanese commercial satellite communications as part of a generation of spacecraft that helped consolidate and expand the country's geostationary fleet during the mid-2000s. Its launch in April 2006 coincided with a period of active restructuring within the Japanese satellite industry, as market consolidation was reshaping how capacity was deployed and managed across the JCSAT and N-STAR networks.

The satellite's continued presence in orbit — it has not reentered or been officially decommissioned in the tracking data available — means it continues to occupy a geostationary slot. Geostationary orbital positions are regulated by the International Telecommunication Union, and maintaining a registered slot requires active coordination. Satellites that have exhausted their propellant and can no longer be controlled are typically moved to a graveyard orbit slightly above the geostationary belt as part of responsible end-of-life disposal practices. Whether JCSAT-5A has been or will be relocated in this manner is not indicated by the available catalog data.

For researchers, engineers, and satellite-tracking enthusiasts, JCSAT-5A represents a well-cataloged Japanese geostationary payload with a clear launch heritage and an unambiguous orbital identity. Its NORAD identifier and COSPAR designator allow it to be located and monitored within standard tracking databases, and its orbital parameters are updated as new observations are processed. The slight inclination of 1.1 degrees gives it a marginally distinct signature compared to perfectly stationkeeping geostationary objects, which may be of minor interest to observers attempting to distinguish closely spaced objects in the geostationary arc.

As a member of the broader JCSAT and N-STAR fleet, the satellite contributed to an era of Japanese communications infrastructure that supported millions of households and businesses receiving satellite television, broadband internet, and related services. Its significance lies less in any singular technical novelty than in its role as a reliable and durable component of a regional communications network that depends on the continuous availability of orbital assets. The A2100 platform on which it was built has itself become a benchmark in commercial satellite design, and JCSAT-5A's operational history — whatever its current service status — adds to the accumulated flight heritage of that platform and of Japanese commercial satellite operations more broadly.

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