IRNSS-1C

NORAD 40269· COSPAR 2014-061A· Active satellite· Communications· GEO
Launch
Launched on Oct 15, 2014 from Satish Dhawan Space Centre First Launch Pad, India aboard a PSLV XL.
PSLV XL | IRNSS-1C
Live · TLE epoch 2026-07-12 21:07 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
Indian Space Research Organisation
Country
India
Manufacturer
Launched
Oct 15, 2014
Mass
1,425 kg
Apogee
35,888 km
Perigee
35,701 km
Inclination
6.58°
Period
23.94 h

About IRNSS-1C

IRNSS-1C is an Indian navigation satellite operating in geostationary orbit, cataloged by NORAD under identifier 40269 and internationally designated 2014-061A. It forms part of India's Indigenous Regional Navigation Satellite System (IRNSS), a constellation developed and operated by the Indian Space Research Organisation (ISRO) to provide positioning and timing services across the Indian subcontinent and surrounding region. As the third satellite in the IRNSS series to be orbited, IRNSS-1C represents an important incremental step in India's effort to build an independent, domestically operated navigational infrastructure.

Mission and Purpose

The IRNSS program was conceived to give India sovereign control over a regional navigation capability, reducing reliance on foreign systems such as the United States' GPS, Russia's GLONASS, or the European Galileo network. Like the systems it was partly designed to complement or substitute, IRNSS was planned as a constellation of satellites that together would deliver continuous navigational coverage to a defined geographic service area centered on India and extending outward across South Asia and the broader Indian Ocean region.

IRNSS-1C is the third satellite to be added to this constellation, following IRNSS-1A and IRNSS-1B, both of which were launched in prior years to begin establishing the network. A complete IRNSS constellation was envisioned to consist of seven operational satellites positioned at carefully chosen orbital slots, enabling the system to achieve the geometric coverage needed for accurate position fixes on the ground. Each satellite in the series plays a designated role within the overall architecture, contributing to the overlapping fields of view that give the system regional reach.

Although the specific mission sub-type carried by IRNSS-1C is not recorded in the public satellite catalog, the IRNSS program as a whole is designed to support both standard positioning services for civilian users and more precise services for authorized users, a dual-tier structure common among regional and global navigation satellite systems. Navigation satellites of this type continuously broadcast ranging signals on multiple radio frequency bands, allowing ground-based receivers to compute their location by measuring signal travel time from several satellites simultaneously.

Orbit and Tracking

IRNSS-1C occupies a near-geostationary orbit, a regime in which satellites circle Earth at an altitude that closely matches the planet's rotation rate, causing them to appear nearly stationary when viewed from the ground. According to current tracking data, the satellite has an apogee of 35,891 km and a perigee of 35,700 km, yielding a very slightly elliptical orbit rather than a perfectly circular one. Its orbital period is 1,436.2 minutes, extremely close to one sidereal day, which is the defining characteristic of a geostationary or near-geostationary orbit.

What distinguishes IRNSS-1C from a purely geostationary communications satellite is its orbital inclination of 6.5 degrees relative to the equatorial plane. A satellite in a true geostationary orbit would have an inclination of zero degrees, holding it fixed directly over the equator and stationary against the sky. With an inclination of 6.5 degrees, IRNSS-1C instead traces a slow figure-eight path, known as an analemma, as seen from any fixed point on the ground. This inclined geosynchronous configuration is a deliberate design choice for navigation satellite constellations, as it allows the satellite to serve higher-latitude regions more effectively than a purely equatorial orbit would permit.

The combination of its high altitude and non-zero inclination means that from the Indian subcontinent, IRNSS-1C appears to wander slightly northward and southward across the sky over the course of each day while remaining broadly in the same area of the sky. Ground tracking antennas designed to work with IRNSS need to accommodate this slow apparent motion rather than treating the satellite as a fixed point.

IRNSS-1C was launched on October 15, 2014, at 00:02 local Indian Standard Time (20:02 UTC on October 14, 2014), aboard a Polar Satellite Launch Vehicle designated PSLV-C26. The PSLV has served as ISRO's reliable workhorse launch vehicle for a wide variety of satellite missions, and its use for the IRNSS series was consistent with ISRO's established launch program at the Satish Dhawan Space Centre. The satellite remains in orbit to this day, with no reentry or decay event recorded.

Design and Operator

IRNSS-1C was built to a mass of 1,425 kg, placing it in the medium-class category for geostationary spacecraft. The satellite's manufacturer is not publicly recorded in the standard catalog entry. It is operated by the Indian Space Research Organisation, the government space agency of India that oversees both the development and operation of Indian civil and scientific space assets.

ISRO, headquartered in Bengaluru, has over several decades grown from a modest national space program into one of the world's significant space agencies, with independent launch capability, a diverse range of Earth observation and communications satellites, and notable interplanetary missions. The development of the IRNSS constellation represents one of ISRO's most strategically significant undertakings, as building a navigation satellite system requires not only the spacecraft themselves but also a dedicated ground control network, precise atomic clock technology, sophisticated signal processing infrastructure, and long-term operational commitment.

Navigation satellites like those in the IRNSS series carry highly stable atomic frequency standards, typically based on rubidium or hydrogen maser technology, since the accuracy of the positioning signal depends fundamentally on the satellite's ability to maintain an extremely precise time reference. The integrity of the timing and broadcasting systems aboard each satellite directly determines how accurately a ground receiver can determine its position. These are demanding technical requirements that place navigation satellite development among the more challenging categories of spacecraft engineering.

Status and Significance

As of the information available in the satellite catalog, IRNSS-1C remains operational in orbit with no reported decay or deorbit event. Its current status in terms of operational health and mission performance is not reflected in the catalog entry, but the satellite has been in orbit for roughly a decade since its 2014 launch.

The IRNSS constellation that IRNSS-1C helped to build has since been operationally named NavIC, an acronym for Navigation with Indian Constellation, and the system has been formally declared operational for its intended service region. NavIC represents one of only a handful of regional or global navigation satellite systems that have achieved operational status worldwide, alongside GPS, GLONASS, Galileo, China's BeiDou, and Japan's QZSS. India's achievement in independently developing and deploying such a system places it in a small group of nations with the technical and industrial capacity to build and sustain a satellite-based navigation infrastructure from the ground up.

IRNSS-1C's contribution as the third satellite in the series was critical to building the constellation to the point where useful positioning geometry began to emerge over the service area. Navigation systems depend on having multiple satellites in view simultaneously, and each successive satellite added to the constellation meaningfully improved the coverage, reliability, and precision available to users on the ground. Without satellites like IRNSS-1C filling out the planned architecture, the overall system could not have achieved the geometric diversity needed for reliable multi-satellite fixes.

From a broader perspective, the IRNSS/NavIC program illustrates how space-based infrastructure has become integral to national strategic planning. Positioning, navigation, and timing services underpin a remarkably wide range of modern activities, from transportation and logistics to precision agriculture, disaster management, military operations, and financial transaction timing. By developing an independent capability in this domain, India reduced a significant point of dependency on foreign-controlled systems whose availability cannot be guaranteed under all geopolitical circumstances.

How to Spot It

IRNSS-1C is not a practical target for casual visual observation. At an orbital altitude of approximately 35,700–35,891 km, it is nearly one hundred times farther from Earth's surface than the International Space Station and far too faint to be seen with the naked eye under any normal circumstances. Even with a modest telescope, detecting a satellite at geostationary altitude requires either a sufficiently large aperture or the use of long-exposure imaging techniques that allow the satellite's faint reflected sunlight to accumulate.

Because of its near-geostationary orbit, IRNSS-1C does not sweep visibly across the sky the way that low Earth orbit satellites do. Instead, it remains approximately fixed in the same region of sky as seen from India and surrounding areas, drifting only slowly through its daily figure-eight pattern. Radio observers and engineers working with satellite tracking equipment may monitor its signals on navigational frequency bands, but for general sky-watching purposes, IRNSS-1C remains invisible without specialized instrumentation.

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