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IRS 1A

NORAD 18960 Payload LEO 1988-021A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
893 km
Apogee
914 km
Inclination
98.8°
Period
103.1 min
Mean Motion
13.97170171 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude904 km
Orbital Velocity26,648 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.97
Eccentricity0.0014
Semi-Major Axis7,275 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
1988-03-17
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1988-021A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IRS 1A is an active satellite operated by India, launched on 1988-03-17 from Baikonur, Kazakhstan. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 893 km and 914 km with an inclination of 98.8°. It travels at approximately 26,648 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.97 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks IRS 1A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IRS 1A orbits at an average altitude of 904 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of IRS 1A’s average altitude, there are currently 211 active payloads and 1,306 tracked debris or rocket body fragments. With an inclination of 98.8°, IRS 1A passes over latitudes between 98.8°N and 98.8°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. India operates approximately 108 active satellites in total, of which 3 share a similar altitude band with IRS 1A.
❓ Frequently Asked Questions
IRS 1A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 904 km altitude. Its 98.8° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 103 minutes, travelling at 26,648 km/h.
IRS 1A is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 18960. You can track IRS 1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRS 1A was launched on 1988-03-17 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRS 1A (NORAD ID 18960) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
IRS 1A travels at approximately 26,648 km/h (16,558 mph) — roughly 7.40 km/s. It completes 13.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.