INSAT-3DS

NORAD 58990· COSPAR 2024-033A· Active satellite· Communications· GEO
Launch
Launched on Feb 17, 2024 from Satish Dhawan Space Centre Second Launch Pad, India aboard a GSLV Mk. II.
GSLV Mk II | INSAT-3DS
INSAT-3DS
Indian Space Research Organisation · GODL-India · via Wikimedia Commons
Live · TLE epoch 2026-07-13 13:51 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
ISRO
Country
India
Manufacturer
Launched
Feb 17, 2024
Mass
Apogee
35,799 km
Perigee
35,791 km
Inclination
0.10°
Period
23.94 h

About INSAT-3DS

INSAT-3DS is an Indian meteorological satellite operated by the Indian Space Research Organisation (ISRO) and placed into geostationary orbit in February 2024. Assigned NORAD catalog identifier 58990 and international designator 2024-033A, it represents a continuation of India's long-running INSAT series of Earth-observation and weather-monitoring spacecraft. The satellite was lofted from the Satish Dhawan Space Centre and has since taken up a position in the geostationary belt, where it contributes to India's national meteorological infrastructure.

Mission and Purpose

INSAT-3DS belongs to a lineage of Indian meteorological satellites that stretches back several decades, forming part of the broader Indian National Satellite System. In practical terms, geostationary meteorological satellites of this class are used for continuous monitoring of weather patterns, cloud cover, sea surface temperatures, atmospheric moisture profiles, and other parameters that feed into numerical weather prediction models. Their fixed vantage point over the same region of Earth—made possible by matching their orbital period precisely to the planet's rotation—allows them to generate frequent imagery of the same geographic area, enabling forecasters to track the evolution of weather systems in near real time.

INSAT-3DS is explicitly a follow-on to the INSAT-3DR mission, inheriting and building on the scientific and operational objectives of that earlier spacecraft. INSAT-3DR itself was designed to provide enhanced meteorological services for India, carrying imaging and sounding instruments capable of profiling the atmosphere in multiple spectral channels. A follow-on mission of this nature typically aims to ensure continuity of service as older satellites age, while incorporating refinements drawn from operational experience with predecessors. In the case of the INSAT series, such satellites serve not only the India Meteorological Department but also broader disaster warning and search-and-rescue support roles, reflecting the dual scientific and humanitarian utility of this class of spacecraft.

The mission type and current operational status are not formally recorded in the public satellite catalog entry for INSAT-3DS. Nonetheless, its classification as a payload in geostationary orbit, combined with its heritage lineage, is consistent with an active meteorological mission serving Indian and regional users.

Orbit and Tracking

INSAT-3DS occupies a geostationary orbit, the class of orbit defined by an altitude and inclination that causes a satellite to appear essentially stationary relative to a point on Earth's surface. The satellite's tracked orbital parameters confirm this classification: its apogee stands at approximately 35,800 km above Earth, and its perigee at approximately 35,789 km, reflecting a very nearly circular orbit at the canonical geostationary altitude. The near-zero difference between apogee and perigee—only about 11 km—indicates an exceptionally well-circularized orbit, as would be expected for an operational geostationary spacecraft following on-orbit maneuvering after launch.

The orbital inclination is recorded at 0.0°, meaning the satellite's orbital plane is aligned essentially perfectly with Earth's equatorial plane. This is the defining geometric feature of a true geostationary orbit: an inclination of zero, combined with the correct altitude, ensures the satellite tracks a fixed longitude above the equator rather than tracing a figure-eight path (known as an analemma) as satellites in inclined geosynchronous orbits do. The orbital period of approximately 1,436.1 minutes—very close to 23 hours and 56 minutes, which is one sidereal day—is the direct consequence of this altitude, reflecting the balance between gravitational pull and orbital velocity at roughly 35,800 km.

For tracking purposes, INSAT-3DS can be identified by its NORAD ID 58990 in standard two-line element (TLE) sets distributed by space surveillance networks. Its international designator, 2024-033A, encodes the fact that it was the primary payload (suffix "A") of the 33rd orbital launch of 2024. Because geostationary satellites maintain a near-fixed position relative to Earth's surface, their ground track is essentially stationary, making them straightforward to point fixed antennas toward but less dramatic objects to track dynamically compared with satellites in low Earth orbit.

The satellite was launched on 17 February 2024 (Indian Standard Time), corresponding to the evening of 16 February 2024 in Coordinated Universal Time. It remains in orbit with no decay or reentry date indicated in the catalog, consistent with an active mission at geostationary altitude, where atmospheric drag is negligible and spacecraft can remain aloft for decades barring mechanical failure or deliberate disposal.

Design and Operator

INSAT-3DS was built and is operated by ISRO, India's primary space agency, which was established in 1969 and has since grown into one of the world's significant space organizations. ISRO has developed the INSAT series over many generations, progressively increasing the capability of its meteorological and communications satellites. The organization manages all aspects of India's satellite programs, from design and manufacturing through launch and operations.

The satellite was launched from the Satish Dhawan Space Centre, located on Sriharikota Island off the coast of Andhra Pradesh in southeastern India. This facility serves as ISRO's primary orbital launch site and has supported launches across the full range of ISRO's launch vehicle family. Details regarding the specific launch vehicle used for this mission are not catalogued in the standard reference data for this entry.

The manufacturer of INSAT-3DS is not recorded in the public catalog entry. Given ISRO's practice of developing and building its own spacecraft domestically, it is widely understood that ISRO acts as both the development agency and operator for satellites in the INSAT meteorological series, though the specific industrial arrangements for any given satellite within the program are not detailed here. The satellite's mass is similarly not publicly listed in the catalog entry for this object.

Significance and Context

The launch of INSAT-3DS in early 2024 added capacity to India's operational meteorological satellite constellation at a time when the demand for high-frequency, high-resolution weather data continues to grow across the subcontinent and surrounding ocean regions. The Indian subcontinent is subject to some of the world's most consequential weather phenomena, including the annual monsoon cycle, tropical cyclones forming in both the Arabian Sea and the Bay of Bengal, and severe convective events that affect hundreds of millions of people. Continuous geostationary coverage from satellites in the INSAT family has become integral to the national weather forecasting and disaster preparedness infrastructure.

As a follow-on to INSAT-3DR, INSAT-3DS contributes to the operational redundancy and long-term continuity of this capability. In satellite meteorology, the principle of maintaining overlapping coverage—where newer spacecraft are in place before older ones reach the end of their design life—is critical to avoiding gaps in the observational record. Weather agencies depend not only on current data but on consistent, well-characterized data streams that allow models to be calibrated and forecasts to be validated over time.

More broadly, INSAT-3DS reflects the maturation of India's indigenous space capability. ISRO has progressively reduced dependence on foreign satellite platforms and launch services across its various programs, and the INSAT meteorological series exemplifies this trajectory. Each successive generation has incorporated lessons from previous satellites and contributed to the institutional knowledge base required to design, build, test, and operate complex geostationary spacecraft.

The satellite's position at geostationary altitude also means it has a potential operational lifespan measured in years or even decades, assuming nominal performance of its onboard systems and sufficient propellant for station-keeping maneuvers. Geostationary spacecraft require periodic thruster firings to counteract gravitational perturbations from the Moon and Sun, which would otherwise cause the orbital inclination to increase over time—pulling the satellite away from its equatorial, fixed-longitude position. The satellite's currently recorded inclination of 0.0° reflects active station-keeping, maintaining the precise orbital slot necessary for continuous Earth observation.

At the end of its operational life, standard practice for geostationary satellites is to maneuver the spacecraft into a slightly higher "graveyard" orbit, above the congested geostationary belt, using whatever propellant remains. This practice helps preserve the limited geostationary arc as a shared resource for the international community of satellite operators. Whether and when INSAT-3DS will eventually be retired in this manner depends on mission outcomes and operational decisions that lie in the future.

In the interim, INSAT-3DS stands as one of the more recent additions to the global network of geostationary weather satellites that collectively provides continuous planetary-scale atmospheric monitoring—a capability that modern meteorology, aviation safety, maritime navigation, and disaster risk reduction all depend upon in fundamental ways.

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