ISRO is preparing to launch GISAT-1A, designated EOS-05, aboard the GSLV-F17 rocket in September 2026.
Unlike conventional remote sensing satellites in low Earth orbit, GISAT-1A will operate from geostationary orbit at about 36,000 km, keeping the Indian landmass continuously in view.
It can image the entire Indian mainland every 30 minutes at 42 metre resolution and revisit designated high-priority areas every 5 minutes.
The payload includes a 700 mm Ritchey-Chretien telescope with multispectral (VNIR) and hyperspectral (VNIR and SWIR) sensors on ISRO's I-2K bus, with a designed life of 10 years.
The mission will also revalidate the GSLV Mk-II and its indigenous cryogenic upper stage, and would be ISRO's first launch since the PSLV-C62/EOS-N1 failure in January 2026.
Almost all Earth observation satellites, including India's Cartosat and RISAT series, fly in low Earth orbit, typically a few hundred kilometres up in a sun-synchronous polar orbit. They see a narrow strip at very fine resolution, but they only pass over a given place once every few days. A geostationary satellite sits about 36,000 km above the equator and circles the Earth in exactly one sidereal day, so from the ground it appears to hang motionless over the same longitude. That buys persistence at the cost of resolution: from that distance the ground sample is 42 metres rather than sub-metre, but the same scene can be revisited every few minutes instead of every few days. For a cyclone tracking eastward, a flood crest moving down a river, or a forest fire spreading through an afternoon, the ability to look again in five minutes is worth far more than extra detail in an image taken three days later.
Simple Analogy: A low Earth orbit satellite is a photographer who walks past your street once a week with a very good camera. A geostationary imager is a CCTV camera bolted to a pole above the neighbourhood: lower detail, but it never looks away.
PSLV, GSLV Mk-II, LVM3 and SSLV form the standard ladder; GSLV Mk-II is the medium-lift vehicle with the CE-7.5 cryogenic upper stage.
India developed the cryogenic upper stage indigenously after technology transfer was blocked in the 1990s, a recurring theme in questions on technology denial regimes.
Disaster management, crop assessment, forest fire detection and coastal monitoring are the standard application set for Indian Earth observation satellites.
Low Earth, sun-synchronous, geostationary, geosynchronous and Molniya orbits, and what each is used for, is high-frequency prelims material.
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A circular equatorial orbit at about 36,000 km where a satellite's period equals one sidereal day, so it appears fixed over one longitude.
How frequently a satellite can revisit and image the same area, as distinct from spatial resolution, which is the smallest feature it can distinguish.
Imaging in many narrow contiguous spectral bands, allowing discrimination of surface mineralogy, crop stress and vegetation condition.
India's indigenous cryogenic engine used in the upper stage of the GSLV Mk-II.