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GSLV-F17 places EOS-05, India's first geosynchronous imaging satellite, in transfer orbit

First brief 4 Sep, 10:55 am IST Updated 4 Sep, 10:55 am IST 2 developments 2 min read Latest ↓
A GSLV launch vehicle during rollout from the assembly building at Sriharikota
Photo: Indian Space Research Organisation / Wikimedia Commons · GODL-India

Where it stands

ISRO launched EOS-05 at 2:55 am on 4 September 2026. The GSLV-F17 rocket lifted off from Sriharikota. The rocket placed EOS-05 in its intended sub-geosynchronous transfer orbit. EOS-05 weighs about 2,367 kg. The spacecraft will next move towards its working geosynchronous orbit. ISRO calls EOS-05 India's first imaging satellite designed for that orbit. The high orbit will let one spacecraft repeatedly observe a large area. EOS-05 is an Earth observation spacecraft. The launch was the 19th flight of the Geosynchronous Satellite Launch Vehicle. The successful insertion begins the satellite's in-orbit commissioning phase.

Background

Most Earth imaging satellites use low or sun-synchronous orbits. Low-orbit satellites pass over the same place at intervals. A geosynchronous satellite completes one orbit in the time Earth takes to rotate once. The satellite can therefore observe the same broad region repeatedly. A transfer orbit is only an intermediate path. The spacecraft uses its own propulsion to raise and shape the final orbit. GSLV uses three stages. The GSLV third stage uses liquid hydrogen and liquid oxygen at very low temperatures.

How it developed

  1. 4 September 2026, 2:55 am
    How it started

    GSLV-F17 lifts off from Sriharikota with the 2,367 kg EOS-05

    GSLV-F17 lifted off at 2:55 am on 4 September 2026. The rocket departed from the second launch pad at Sriharikota. The rocket carried the 2,367 kg EOS-05 Earth observation spacecraft.

  2. 4 September 2026, about 18 minutes after lift-off
    New fact

    Rocket places EOS-05 in the intended sub-geosynchronous transfer orbit

    GSLV-F17 placed EOS-05 in its intended orbit after lift-off. The nominal transfer orbit has a 170 km perigee and a 28,934 km apogee. The elliptical path is not the satellite's final working orbit.

  3. 4 September 2026
    Consequence

    EOS-05 becomes India's first imaging satellite for geosynchronous orbit

    ISRO describes EOS-05 as a state-of-the-art Earth observation spacecraft. EOS-05 is India's first imaging satellite designed for geosynchronous orbit. The successful insertion starts the spacecraft's journey towards its working orbit.

Why it matters for UPSC

GS3 · Space technologyGS3 · Earth observationPrelims · Orbits and launch vehicles

For GS3, separate the launch vehicle from the satellite. GSLV-F17 carried EOS-05. EOS-05 performs Earth observation. Also separate a transfer orbit from the working orbit. The rocket placed EOS-05 in a sub-geosynchronous transfer orbit. The spacecraft must later raise its orbit. For Prelims, remember one distinction. Every geostationary orbit is geosynchronous. A geosynchronous orbit need not appear fixed over one point. A geostationary orbit must be circular and above the equator.

Key terms

Geosynchronous Satellite Launch Vehicle (GSLV)GSLV is an Indian launch vehicle for placing heavier satellites into high transfer orbits. GSLV-F17 was the 19th GSLV flight. The rocket is 51.7 metres high and has three stages. The lift-off mass was about 420.5 tonnes. The final CUS15 stage is cryogenic.
Geosynchronous orbitA satellite in geosynchronous orbit takes one sidereal day to circle Earth. A sidereal day is about 23 hours and 56 minutes. The satellite returns to the same position in the sky at the same time each day. A geosynchronous path need not be circular or directly above the equator.
Geostationary orbitA geostationary orbit is a special geosynchronous orbit. The orbit is circular and lies above the equator. The satellite moves in the same direction as Earth's rotation. The satellite therefore appears fixed above one longitude.
Sub-geosynchronous transfer orbitA transfer orbit is an intermediate elliptical orbit. GSLV-F17 placed EOS-05 in a sub-geosynchronous transfer orbit. ISRO's nominal figures were a 170 km perigee and a 28,934 km apogee. EOS-05 must use onboard propulsion to move towards its working orbit.
Earth observation satelliteAn Earth observation satellite collects images or measurements of Earth's land, water and atmosphere. Governments use such data for mapping, resource management, weather services and disaster response. EOS-05 is India's first imaging satellite designed to work from geosynchronous orbit.
Cryogenic upper stageA cryogenic stage burns propellants stored at extremely low temperatures. The GSLV CUS15 stage uses liquid hydrogen and liquid oxygen. Cryogenic propulsion gives the upper stage the efficiency needed for high-energy satellite missions.
Sources (4)
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