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IMS-1

NORAD 32786 Payload LEO 2008-021D ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
548 km
Apogee
555 km
Inclination
98.0°
Period
95.7 min
Mean Motion
15.05021834 rev/day
TLE Epoch
2026-09-17 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude552 km
Orbital Velocity27,317 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.05
Eccentricity0.0005
Semi-Major Axis6,923 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇳 ISRO (India)
Launch Date
2008-04-28
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2008-021D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
IMS-1 is an active satellite operated by ISRO (India), launched on 2008-04-28 from Satish Dhawan Space Centre, India on the PSLV Rideshare 01 launch. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 548 km and 555 km with an inclination of 98.0°. It travels at approximately 27,317 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.05 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks IMS-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IMS-1 orbits at an average altitude of 552 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 IMS-1’s average altitude, there are currently 1,688 active payloads and 407 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 9% of all active satellites. With an inclination of 98.0°, IMS-1 passes over latitudes between 98.0°N and 98.0°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 109 active satellites in total, of which 19 share a similar altitude band with IMS-1.
❓ Frequently Asked Questions
IMS-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 552 km altitude. Its 98.0° 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 96 minutes, travelling at 27,317 km/h.
IMS-1 is operated by ISRO (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 32786. You can track IMS-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IMS-1 was launched on 2008-04-28 from Satish Dhawan Space Centre, India, India’s primary launch facility on a barrier island off the coast of Andhra Pradesh. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks IMS-1 (NORAD ID 32786) 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.
IMS-1 travels at approximately 27,317 km/h (16,974 mph) — roughly 7.59 km/s. It completes 15.05 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.