GSAT-14

NORAD 39498· COSPAR 2014-001A· Active satellite· Communications· GEO
Launch
Launched on Jan 5, 2014 from Satish Dhawan Space Centre Second Launch Pad, India aboard a GSLV Mk. II.
GSLV Mk II | GSAT-14
Live · TLE epoch 2026-07-13 13:48 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
Indian Space Research Organisation
Country
India
Manufacturer
OHB
Launched
Jan 5, 2014
Mass
1,982 kg
Apogee
35,803 km
Perigee
35,787 km
Inclination
0.02°
Period
23.94 h

About GSAT-14

GSAT-14 is an Indian geostationary communications satellite operated by the Indian Space Research Organisation (ISRO). Launched in early January 2014, it represents one of a long series of GSAT-series spacecraft that have progressively expanded India's domestic satellite communications infrastructure. The satellite carries the NORAD catalog identifier 39498 and the international designator 2014-001A, reflecting its status as the first tracked object cataloged from launches in that year. As of the time of writing, GSAT-14 remains operational in geostationary orbit above the equator.

Mission and Purpose

GSAT-14 was developed to serve India's growing demand for satellite-based telecommunications services. Within the GSAT program, it was positioned as a successor to GSAT-3, an earlier communications satellite that had been in service since 2004, with GSAT-14 effectively stepping into its role and relieving pressure on aging orbital assets.

The specific payload details and active mission parameters are not fully documented in publicly available tracking catalogs — mission type and current operational status are listed as unknown in standard orbital databases. What is broadly understood is that the GSAT series as a whole supports a range of applications including direct-to-home television broadcasting, telecommunications relay, and various governmental and commercial communications needs across the Indian subcontinent and surrounding regions. GSAT-14 fits within that broader context of expanding India's sovereign space-based communications capacity.

The satellite's development was driven, at least in part, by ISRO's long-standing objective to reduce dependence on foreign launch vehicles and foreign satellite infrastructure. By fielding successive GSAT satellites on domestically developed launch vehicles and with growing domestic manufacturing involvement, ISRO has used each mission as both a practical communications asset and a testbed for indigenous technology.

Orbit and Tracking

GSAT-14 occupies a near-perfect geostationary orbit, with an apogee of approximately 35,799 kilometers and a perigee of approximately 35,791 kilometers above Earth's surface. The difference between these two figures is remarkably small — less than ten kilometers — indicating an orbit that is very close to circular. Its inclination is recorded as 0.0 degrees, meaning the satellite's orbital plane lies essentially flush with Earth's equatorial plane. These characteristics together define the classical geostationary slot: the satellite remains fixed relative to the rotating Earth, appearing stationary when viewed from the ground.

The orbital period of GSAT-14 is approximately 1,436.2 minutes, or just under 24 hours, which is precisely what is required to remain synchronous with Earth's rotation. This near-perfect match between orbital period and Earth's rotation rate is what allows geostationary satellites to maintain a fixed position in the sky as seen from any point on the ground within their field of view.

With a mass of 1,982 kilograms at launch, GSAT-14 is a mid-sized communications satellite by contemporary standards, though substantial enough to carry meaningful telecommunications payloads. Its geostationary altitude places it far beyond low Earth orbit and well above even medium Earth orbit regimes, at a distance from the surface roughly equivalent to traveling three times around the Earth's circumference.

From a tracking perspective, GSAT-14 is cataloged under NORAD ID 39498. Its highly stable, near-equatorial orbit means that its position is predictable with exceptional precision. Unlike satellites in lower or more eccentric orbits, GSAT-14 does not drift appreciably relative to the Earth's surface and does not experience the kind of rapid positional changes that make tracking complex for, say, a low Earth orbit spacecraft.

Design and Operator

GSAT-14 was manufactured by OHB, the German-headquartered space technology company, and was built on behalf of the Indian Space Research Organisation. The involvement of an established European commercial satellite manufacturer reflects the international dimension of India's space program — even as ISRO has worked toward greater indigenous capability, it has also engaged with global industry partners where appropriate to meet mission requirements and timelines.

ISRO, headquartered in Bengaluru, India, is the primary governmental space agency of India and operates under the Department of Space. It has been responsible for a large and growing fleet of operational satellites spanning communications, remote sensing, meteorology, and navigation. The GSAT series represents ISRO's main line of geostationary communications satellites, and GSAT-14 is one of the more notable entries in that series given the launch circumstances surrounding its deployment.

The satellite was lofted into orbit on January 5, 2014 (converted from the UTC-offset launch timestamp), aboard a Geosynchronous Satellite Launch Vehicle in its Mk.II configuration. That particular version of the GSLV is significant in the context of Indian space history because it incorporated a cryogenic upper stage that was designed and built domestically within India. Cryogenic rocket engines, which use liquid hydrogen and liquid oxygen as propellants, are among the most technically demanding components in launch vehicle engineering. India's development of an indigenous cryogenic engine represented a substantial long-term investment in launch technology, and the GSLV Mk.II mission carrying GSAT-14 was one of the early demonstrations of that capability being applied to an operational payload. The use of a cryogenic third stage is essential for delivering satellites of meaningful mass to geostationary transfer orbit, and its reliable performance on this mission was a meaningful milestone for the Indian launch vehicle program.

Significance and Legacy

The GSAT-14 mission sits at an intersection of several important threads in India's spacefaring ambitions. First, it addressed a direct operational need: replacing aging geostationary capacity previously provided by GSAT-3, ensuring continuity of service for communications applications that depend on satellites stationed over the Indian Ocean region. Second, it served as a validation flight for the GSLV Mk.II with its domestically developed cryogenic engine, demonstrating that India could field a heavy-lift geostationary launch capability without reliance on foreign upper stages.

For much of the preceding decade, India's efforts to develop a cryogenic engine had faced significant technical obstacles, and earlier GSLV flights had experienced setbacks. The successful deployment of GSAT-14 to its intended orbit was therefore not simply a routine communications satellite launch — it carried with it the weight of years of development effort and the importance of demonstrating that the GSLV Mk.II had matured into a dependable vehicle. A successful mission bolstered confidence in the platform and laid groundwork for subsequent, more ambitious GSLV missions.

From a geopolitical standpoint, the ability to independently launch communications satellites of this mass class to geostationary orbit is strategically significant. Countries and agencies that depend entirely on foreign launch providers for access to geostationary orbit are subject to commercial and political constraints that can complicate or delay satellite deployment. ISRO's continued development of domestic launch capacity, of which the GSLV Mk.II and GSAT-14's launch is a part, reflects a deliberate national policy of maintaining sovereign access to space.

GSAT-14 remains in orbit as of the current catalog data, with no decay or reentry date recorded. Geostationary satellites are routinely expected to have operational lifespans measured in years to well over a decade, after which they are typically maneuvered to a slightly higher "graveyard" orbit to vacate their geostationary slot for successor spacecraft. Whether GSAT-14 has reached end of operational life or continues to support active services is not reflected in the public orbital catalog record, which notes mission status as unknown.

The satellite's continued presence in the geostationary belt is consistent with the typical trajectory of such assets. Its catalog entry continues to be maintained by NORAD and associated tracking agencies, preserving a permanent record of its presence as part of humanity's growing inventory of space objects. With an essentially circular equatorial orbit and no sign of reentry, GSAT-14 will likely remain a stable occupant of the geostationary arc for the foreseeable future, whether as an active communications relay, a dormant asset, or eventually a decommissioned object awaiting final disposal maneuvers.

How to Spot It

GSAT-14 is not generally observable by amateur skywatchers using the naked eye or small telescopes under typical conditions. At a distance of roughly 35,800 kilometers from Earth's surface, geostationary satellites are vastly farther away than the low-orbit spacecraft — such as the International Space Station — that are routinely watched by satellite observers. While optical tracking of geostationary satellites is technically possible with larger telescopes and long-exposure astrophotography, it requires deliberate effort and equipment beyond what casual observers use.

From a ground observer's perspective, GSAT-14 would appear essentially stationary against the background stars, distinguishable from a star only by its position and the fact that it reflects sunlight rather than generating its own. It would appear near the celestial equator at the longitude corresponding to its assigned geostationary slot. Dedicated tracking tools, including the orbital elements maintained in real time on this site, can confirm its precise apparent position for observers wishing to attempt a telescopic observation or optical verification.

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