🗞️ Why in News On the evening of 7 September 2026 the Indian Space Research Organisation completed the third and final orbit-raising manoeuvre on EOS-05, an Earth imaging satellite launched by GSLV-F17 at 02:55 IST on 4 September 2026 from the Second Launch Pad at the Satish Dhawan Space Centre, Sriharikota. The final burn of the satellite’s Liquid Apogee Motor lasted 1,247 seconds and left it in an orbit of about 34,903 km by 35,884 km, close to its operational slot at 85.5 degrees East. EOS-05 is India’s first Earth imaging satellite designed to operate from geosynchronous orbit. It is also the operational successor to EOS-03 / GISAT-1. That background matters: EOS-03 was lost in the GSLV-F10 launch failure of 12 August 2021, when the cryogenic upper stage failed.

What EOS-05 Is, and Why the Orbit is the Story

Earth imaging satellites can be sorted by the orbit they occupy far more usefully than by the sensor they carry. The orbit fixes the physics of what the satellite can and cannot do.

Most Indian civilian remote sensing satellites, from the Cartosat series to the Resourcesat and Oceansat series, sit in sun-synchronous polar orbit (SSO) at altitudes of about 500 to 900 km. A polar orbit passes close to both poles on each revolution, and the sun-synchronous variant is tuned so that the satellite crosses every point at the same local solar time on each visit. This gives consistent illumination and very high spatial resolution, at the cost of a long revisit interval, typically several days for a single point on the ground.

EOS-05 does the opposite trade. It is being placed into geosynchronous orbit (GEO), at an altitude of about 35,786 km, from where it can stare continuously at the same region rather than revisiting it once every few days. Persistence replaces resolution. The cost is that a sensor at 36,000 km cannot resolve features on the ground as sharply as a Cartosat at 500 km.

Orbit Altitude Best at Trade-off
Sun-synchronous polar 500 to 900 km High spatial resolution, consistent illumination Long revisit; the satellite only sees a point when it passes over
Geosynchronous about 35,786 km Continuous coverage of the same region, near-real-time monitoring Coarser spatial resolution from a far greater altitude

Why persistence matters for India. A cyclone track, a forest fire, a cloudburst over the Himalayas, a chemical plume drifting off the coast: none of these wait a week for the next satellite pass. A geosynchronous imager can watch the event unfold, minute by minute, over the same footprint. That is the class of capability EOS-05 introduces to India’s civilian remote sensing constellation.

Geosynchronous is Not the Same as Geostationary

A geosynchronous orbit has a period of one sidereal day, about 23 hours 56 minutes 4 seconds, matching Earth’s rotation. A geostationary orbit is the special case of a geosynchronous orbit that also lies exactly in the equatorial plane and has zero eccentricity, so the satellite appears fixed relative to a point on the equator.

Geosynchronous but inclined or slightly eccentric orbits trace a figure-of-eight, or analemma, in the sky as seen from the ground. INSAT communications and meteorological satellites, and Cartosat-3’s imaging heritage aside, this is the orbital regime that ISRO has traditionally used for weather monitoring through the INSAT-3D and INSAT-3DR series.

The Sensor Payload

The principal payload of EOS-05 is a 700 mm Ritchey-Chretien telescope, carried on a modified I-2K satellite bus, feeding both multispectral and hyperspectral detector arrays. The arrays work across the visible and near-infrared (VNIR) and short-wave infrared (SWIR) regions, with the multispectral channels imaging at the finest ground resolution and the hyperspectral channels, which slice the spectrum into far more numerous and narrower bands, imaging at a coarser one.

The distinction matters for the exam, because it is the trade-off that defines the satellite.

  • Multispectral imaging uses a handful of broad bands and gives the sharper picture.
  • Hyperspectral imaging uses hundreds of narrow contiguous bands and gives a spectral signature for each pixel, which is what allows a crop, a mineral or a pollutant to be identified rather than merely seen. The cost is spatial resolution.

What the geosynchronous vantage adds is not sharpness but persistence. From about 36,000 km the satellite holds the same broad region in view continuously, so it can revisit a selected area roughly every five minutes and image the entire Indian landmass in roughly thirty minutes. A polar-orbiting imager, however sharp, passes over a given point only briefly and returns days later.

That persistence is what makes the satellite useful for cyclone tracking, flood inundation mapping as it develops, forest fire detection, agricultural stress monitoring and rapid damage assessment after a disaster, where the value lies in watching a situation change through the day rather than in one high-resolution snapshot.

⚠️ A trap worth marking. EOS-05 is an optical and infrared imager. Optical, near-infrared and short-wave infrared instruments cannot see through cloud. Only synthetic aperture radar (SAR), an active microwave sensor of the kind carried by the RISAT series and by EOS-04, images through cloud cover and at night regardless of illumination. Do not attribute all-weather capability to EOS-05.

The Launcher: GSLV-Mk-II, and Why Its Reliability is a Story

GSLV-F17 was the nineteenth flight of the Geosynchronous Satellite Launch Vehicle, in its Mk-II configuration with an indigenous cryogenic upper stage. This is the launcher India built precisely so that heavy communications and geosynchronous-class payloads would not depend on foreign upper stages or foreign launches.

Its record has been a mixed one, and the 2025-26 setbacks are worth stating plainly.

GSLV episode What happened
GSLV-F10, 12 August 2021 Cryogenic upper stage failed; EOS-03 / GISAT-1 lost. EOS-05 is the operational replacement.
PSLV third-stage failure, May 2025 A PSLV-C mission suffered a third-stage anomaly, disrupting a scheduled payload delivery.
PSLV third-stage failure, January 2026 A second PSLV third-stage anomaly compounded the concern about upper-stage reliability across ISRO’s workhorse launchers.
GSLV-F17, 4 September 2026 Successful lift-off with EOS-05 from the Second Launch Pad, Sriharikota, at 02:55 IST. At 2,367 kg, the heaviest satellite GSLV has placed into a geosynchronous transfer orbit.

Two PSLV third-stage failures inside eight months, on a launcher whose reliability record was ISRO’s strongest asset, was the reliability question of the year. A national-level expert committee traced both to the third-stage propulsion system; modified components were validated in ground tests, and ISRO announced in July 2026 that the anomaly stood resolved and launches could resume. GSLV-F17’s success sits alongside that clearance rather than in place of it, because PSLV and GSLV are separate programmes.

Sub-Geosynchronous Transfer Orbit is Not Geosynchronous Orbit

A frequent Prelims trap. The GSLV placed EOS-05 into a sub-geosynchronous transfer orbit (sub-GTO) about eighteen minutes after lift-off, not directly into its final geosynchronous slot. The satellite then raised itself, over successive burns of its Liquid Apogee Motor (LAM), from the transfer ellipse towards a near-circular geosynchronous orbit at about 35,786 km. The nomenclature matters: the launcher inserts a satellite into a transfer orbit; the satellite raises itself into the working orbit.

That campaign ran across three manoeuvres in the days after launch.

Manoeuvre Completed LAM burn Resulting orbit
First 5 September 2026, 20:19 IST 5,406.4 seconds 20,000 km x 31,129 km
Third and final 7 September 2026, 20:57 IST 1,247 seconds 34,903 km x 35,884 km

The satellite is now being drifted to its operational geosynchronous slot at 85.5 degrees East, with spacecraft health reported normal.

Strategic and Operational Uses

The uses to which a persistent Indian geosynchronous imager can be put are genuinely broad, and they cut across civilian, security and disaster-management domains.

  • Disaster monitoring and response. Continuous coverage of a developing cyclone, cloudburst or forest fire is qualitatively different from a delayed post-event image.
  • Border and maritime surveillance. Persistent stare over regions of interest, without waiting for the next pass, is the class of capability the Indian defence establishment has publicly identified as a gap.
  • Weather and climate. Complements the INSAT-3D and INSAT-3DR series with additional infrared sensing capacity.
  • Agriculture. Wide-area, high-frequency thermal mapping of the Indo-Gangetic plain and the peninsular cropping zones during sowing and harvest.
  • Forest and land management. Fire detection, vegetation stress and land-cover change at the regional scale.

Where EOS-05 Fits in ISRO’s Earth Observation Family

Satellite series Purpose Orbit Typical resolution
Cartosat High-resolution cartographic imaging Sun-synchronous polar Sub-metre to a few metres
Resourcesat Land use, agriculture, vegetation Sun-synchronous polar 5.8 m and coarser
Oceansat Ocean colour, sea surface temperature Sun-synchronous polar Coarser resolutions optimised for ocean use
RISAT Synthetic aperture radar imaging (all-weather, day-night) Sun-synchronous polar Sub-metre to metres depending on mode
INSAT-3D, 3DR Meteorology, atmospheric sounding Geosynchronous Weather imaging, not high-resolution Earth imaging
EOS-05 Continuous Earth imaging Geosynchronous Coarser than polar imagers, traded for persistence

EOS-05 does not compete with Cartosat. It does something Cartosat cannot: it does not have to leave.

UPSC Relevance

GS Paper 3. Awareness in space; developments in indigenous technology; applications of space technology in national development, disaster management and security.

The Mains framing. The strongest line for a Mains answer is that India’s civilian Earth observation programme was built for the polar-orbit paradigm, where the trade is high resolution against long revisit times, and that a geosynchronous imager introduces a qualitatively different capability, of persistence rather than sharpness. The two are complementary, not rivals. A sophisticated answer will pair EOS-05 with the reliability question raised by two PSLV third-stage failures in eight months, and note that indigenous heavy-lift reliability is now itself an examinable subject.

Prelims focus. Difference between geosynchronous and geostationary orbits; that sub-GTO is a transfer orbit and not the working orbit; the payload is a 700 mm Ritchey-Chretien telescope with multispectral and hyperspectral VNIR and SWIR arrays, not a synthetic aperture radar, so it does not see through cloud; the 85.5 degrees East slot; EOS-05 replaces EOS-03 / GISAT-1 lost in 2021; GSLV-F17 was the 19th GSLV flight and EOS-05 at 2,367 kg its heaviest GTO payload; the launch pad was the Second Launch Pad at Sriharikota; INSAT-3D and INSAT-3DR are the geosynchronous meteorological satellites, distinct from the Earth observation family.

📌 Facts Corner — Knowledgepedia

Prelims, statement-ready facts:

  • EOS-05 is India’s first Earth imaging satellite designed to operate from geosynchronous orbit.
  • It was launched by GSLV-F17 at 02:55 IST on 4 September 2026 from the Second Launch Pad at the Satish Dhawan Space Centre, Sriharikota.
  • At 2,367 kg, EOS-05 is the heaviest satellite GSLV has placed into a geosynchronous transfer orbit.
  • EOS-05 is the operational replacement for EOS-03, also known as GISAT-1, lost when the GSLV-F10 cryogenic upper stage failed on 12 August 2021.
  • The launcher placed EOS-05 into a sub-geosynchronous transfer orbit about 18 minutes after lift-off.
  • The satellite then raised itself towards the near-circular geosynchronous orbit using its own Liquid Apogee Motor.
  • The third and final orbit-raising manoeuvre was completed on 7 September 2026 at 20:57 IST, leaving an orbit of about 34,903 km by 35,884 km.
  • The operational geosynchronous slot for EOS-05 is 85.5 degrees East.
  • The principal payload is a 700 mm Ritchey-Chretien telescope on a modified I-2K bus.
  • It feeds multispectral and hyperspectral arrays in the visible, near-infrared and short-wave infrared regions.
  • From geosynchronous altitude EOS-05 can revisit a selected area about every five minutes and cover the Indian landmass in about thirty minutes.
  • GSLV-F17 was the 19th flight of the GSLV, in its Mk-II configuration with the indigenous cryogenic upper stage.
  • A geosynchronous orbit has a period of one sidereal day, at an altitude of about 35,786 km.
  • A geostationary orbit is the special case of a geosynchronous orbit that is equatorial and circular; the satellite appears fixed above a point on the equator.
  • Most Indian civilian Earth observation satellites, including Cartosat, Resourcesat and Oceansat, operate in sun-synchronous polar orbit at 500 to 900 km altitude.
  • India’s geosynchronous meteorological satellites are the INSAT-3D and INSAT-3DR series.

Prelims, the traps:

  • Sub-geosynchronous transfer orbit is a transfer orbit, not the working orbit. The launcher places the satellite there; the satellite raises itself into the working orbit.
  • Geosynchronous and geostationary are not the same. Every geostationary orbit is geosynchronous; not every geosynchronous orbit is geostationary.
  • EOS-05 is an optical and infrared imager, not a synthetic aperture radar, so it cannot see through cloud. The RISAT series and EOS-04 carry SAR, which can.
  • Multispectral means a few broad bands at finer resolution; hyperspectral means hundreds of narrow contiguous bands at coarser resolution. EOS-05 carries both.
  • The persistence advantage of geosynchronous imaging comes at the cost of spatial resolution. Persistent stare and sub-metre resolution cannot both be delivered from a single satellite.
  • GSLV-F10 in August 2021 lost EOS-03 / GISAT-1. GSLV-F17 in September 2026 launched EOS-05. They are separate missions and separate satellites.

Source: EOS-05, India's First Geosynchronous Earth Imaging Satellite — Ujiyari.com | Free UPSC & State PCS Current Affairs