IRS 1D
NORAD 24971
Payload
LEO
1997-057A
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LEO · NORAD 24971
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
737 km
Apogee
810 km
Inclination
98.8°
Period
100.3 min
Mean Motion
14.35514522 rev/day
TLE Epoch
2026-06-18 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude774 km
Orbital Velocity26,890 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.36
Eccentricity0.0051
Semi-Major Axis7,145 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
1997-09-29
Launch Site
SRI
Int'l Designator
1997-057A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IRS 1D is an active satellite operated by India, launched on 1997-09-29 from SRI. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 737 km and 810 km with an inclination of 98.8°. It travels at approximately 26,890 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.36 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 ~25–100 years. Orbital Radar tracks IRS 1D 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 1D orbits at an average altitude of 774 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 1D’s average altitude, there are currently 386 active payloads and 2,117 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 98.8°, IRS 1D 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 12 share a similar altitude band with IRS 1D.
❓ Frequently Asked Questions
IRS 1D is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 774 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 100 minutes, travelling at 26,890 km/h.
IRS 1D is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24971. You can track IRS 1D in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRS 1D was launched on 1997-09-29 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRS 1D (NORAD ID 24971) 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 1D travels at approximately 26,890 km/h (16,708 mph) — roughly 7.47 km/s. It completes 14.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.