IRS P6
NORAD 28051
Payload
LEO
2003-046A
● Active
CONNECTING…
LEO · NORAD 28051
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
726 km
Apogee
817 km
Inclination
98.2°
Period
100.3 min
Mean Motion
14.36163022 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude772 km
Orbital Velocity26,893 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.36
Eccentricity0.0064
Semi-Major Axis7,143 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇮🇳 Indian Space Research Organization (ISRO) (India)
Launch Date
2003-10-17
Launch Site
SRI
Int'l Designator
2003-046A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IRS P6 is an active satellite operated by Indian Space Research Organization (ISRO) (India), launched on 2003-10-17 from SRI. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 726 km and 817 km with an inclination of 98.2°. It travels at approximately 26,893 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 P6 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 P6 orbits at an average altitude of 772 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 P6’s average altitude, there are currently 386 active payloads and 2,110 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 98.2°, IRS P6 passes over latitudes between 98.2°N and 98.2°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 P6.
❓ Frequently Asked Questions
IRS P6 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 772 km altitude. Its 98.2° 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 26,893 km/h.
IRS P6 is operated by Indian Space Research Organization (ISRO) (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28051. You can track IRS P6 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRS P6 was launched on 2003-10-17 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 P6 (NORAD ID 28051) 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 P6 travels at approximately 26,893 km/h (16,711 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.