JCSAT-2B

NORAD 41471· COSPAR 2016-028A· Active satellite· Communications· GEO
Launch
Launched on May 6, 2016 from Space Launch Complex 40, United States of America aboard a Falcon 9 Full Thrust.
Falcon 9 Full Thrust | JCSAT-14
Live · TLE epoch 2026-07-13 12:13 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
SKY Perfect JSAT Holdings
Country
Japan
Manufacturer
Lanteris Space Systems
Launched
May 6, 2016
Mass
Apogee
35,798 km
Perigee
35,792 km
Inclination
0.02°
Period
23.94 h

About JCSAT-2B

JCSAT-2B is a Japanese geostationary communications satellite operated by SKY Perfect JSAT Holdings, one of Asia's leading satellite communications providers. Launched on May 5, 2016, the spacecraft has been stationed in geostationary orbit ever since, delivering broadband and broadcast services across a wide coverage footprint. It is catalogued in the NORAD system under ID 41471 and carries the international designator 2016-028A, reflecting its status as the primary payload of its launch vehicle's 28th orbital mission of 2016.

Mission and Purpose

JCSAT-2B serves as a commercial communications relay platform, extending the reach of SKY Perfect JSAT's network across the Asia-Pacific region and beyond. The satellite carries a mixed payload of C-band and Ku-band transponders — 26 and 18 respectively — together providing a total bandwidth of approximately 2,853 MHz. This combination of frequency bands allows the satellite to serve a broad range of customers and use cases. C-band transponders, which operate at lower microwave frequencies and are less susceptible to rain fade, are well suited to broadcast distribution and maritime or aeronautical applications across wide geographic areas. Ku-band transponders, operating at higher frequencies, support direct-to-home television broadcasting and data services where smaller ground terminals are preferred.

The satellite was known prior to entering service as JCSAT-14, a designation used during its construction and pre-launch period by the operator. Upon successful commissioning following launch and in-orbit testing, it was renamed JCSAT-2B, taking its place within SKY Perfect JSAT's operational fleet. The mission type and current operational status are not publicly detailed in the satellite catalog record, though the satellite remains in orbit and continues to be tracked.

Orbit and Tracking

JCSAT-2B occupies a geostationary orbit, the band of space approximately 35,786 kilometers above Earth's equator where a satellite's orbital period naturally matches the planet's rotation. Objects in this regime appear essentially stationary when observed from the ground, making them ideal for continuous communications relay without the need for complex tracking systems at ground stations.

The satellite's current orbital parameters reflect a well-maintained geostationary position. Its apogee stands at 35,801 kilometers and its perigee at 35,790 kilometers, giving an orbit that is nearly perfectly circular with a difference of only 11 kilometers between the high and low points. This near-zero eccentricity is characteristic of an actively controlled operational satellite, as operators regularly perform station-keeping maneuvers using onboard propulsion to counteract the gravitational perturbations caused by the Moon, Sun, and Earth's own irregular mass distribution. The orbital inclination is recorded at 0.0°, confirming that the spacecraft sits directly above the equatorial plane — a prerequisite for true geostationary operation. The orbital period of 1,436.2 minutes is effectively synchronous with Earth's sidereal rotation.

JCSAT-2B is tracked continuously by the United States Space Surveillance Network, and its orbital elements are published through space-track.org and redistributed across satellite tracking platforms. Because geostationary satellites do not drift rapidly across the sky, their tracking positions update more slowly than those of low-Earth-orbit objects, but precise element maintenance remains important for interference avoidance and conjunction analysis with neighboring geostationary assets.

Design and Operator

The satellite was manufactured by Lanteris Space Systems and is built on the SSL 1300 platform, a widely used commercial satellite bus with a long heritage in geostationary telecommunications missions. The SSL 1300 bus is designed to accommodate a diverse range of payload configurations and has been adapted for high-power, high-capacity satellites of the class that JCSAT-2B represents. The spacecraft had a launch mass of approximately 4,696 kilograms, reflecting the substantial fuel load required for geostationary transfer orbit injection and years of station-keeping. At end of life, the satellite is designed to produce between 9 and 9.9 kilowatts of electrical power, sufficient to drive its full complement of transponders. Its design life is 15 years, placing its nominal operational horizon around 2031 if launched in 2016, though satellites of this class frequently continue to provide useful service beyond their initial design period when fuel permits.

SKY Perfect JSAT Holdings, headquartered in Japan, is the operator of record for JCSAT-2B. The company is one of the largest satellite operators in the Asia-Pacific region, managing a fleet of geostationary spacecraft that collectively serve broadcast, broadband, maritime, and government customers. SKY Perfect JSAT was formed through the merger of JSAT Corporation and SkyPerfecTV! and has since expanded its footprint significantly. JCSAT-2B fits within a broader strategy of replacing and augmenting older orbital assets to maintain continuous service across the company's coverage areas.

The satellite's launch in May 2016 was notable in the context of commercial spaceflight not only for the payload it carried but also for the nature of its launch vehicle mission. The flight was conducted by SpaceX on a Falcon 9 rocket, and the mission is often remembered in spaceflight history for the successful return and landing of the rocket's first stage — a demonstration that came despite the demanding trajectory required for the high-energy geostationary transfer orbit insertion that JCSAT-2B's mission required. The first stage booster performed a so-called "deep space" return, arriving at the landing zone with minimal propellant margins, and its successful recovery was considered a significant milestone in reusable launch vehicle development.

Current Status and Significance

As of the time of writing, JCSAT-2B remains in orbit and continues to be catalogued as an active payload by the Space Surveillance Network. No decay or reentry date has been recorded, consistent with a satellite maintained in geostationary orbit under active station-keeping. Geostationary satellites of this class are typically deorbited at end of life into a "graveyard" or disposal orbit several hundred kilometers above the geostationary belt, in accordance with international guidelines designed to preserve the geostationary arc for future operators. Whether JCSAT-2B has reached or is approaching that phase of its life is not reflected in the publicly available catalog data reviewed here.

JCSAT-2B represents a class of large commercial communications satellites that have underpinned Asia-Pacific broadcast and data infrastructure for decades. The high-throughput design of the satellite — combining multiple frequency bands with substantial total bandwidth — positions it as a versatile asset capable of serving both legacy broadcast customers and newer broadband applications. In the broader context of SKY Perfect JSAT's operations, JCSAT-2B is one of several geostationary satellites that together provide the coverage depth and redundancy required by commercial and government customers operating across the Pacific basin.

The satellite's association with the SpaceX Falcon 9 mission that launched it has also given it a footnote in the history of the commercial launch industry, independent of its operational communications role. As one of the payloads used to demonstrate high-performance geostationary delivery by a new generation of partially reusable launch vehicles, JCSAT-2B's mission contributed to the validation of a launch architecture that has since become dominant in the commercial market.

For researchers, operators, and satellite enthusiasts, JCSAT-2B can be identified at any time by its NORAD catalog ID 41471 or its COSPAR designation 2016-028A, and its orbital elements can be retrieved from standard two-line element set repositories. Given its geostationary position and near-zero inclination, the satellite remains essentially fixed above the equator as seen from the ground, appearing at a consistent point in the sky from any given location in its coverage footprint throughout its operational life.

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