Skip to content
Home Library Satellite Directory INSAT 3E

INSAT 3E

NORAD 27951 Payload GEO 2003-043E ● Active
CONNECTING… GEO · NORAD 27951
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35586 km
Apogee
35688 km
Inclination
9.7°
Period
1428.5 min
Mean Motion
1.00806405 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,637 km
Orbital Velocity11,089 km/h
Velocity3.08 km/s
Orbital Period23 hours 48 minutes
Orbits / Day1.01
Eccentricity0.0012
Semi-Major Axis42,008 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2003-09-27
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2003-043E
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 3E is an active satellite operated by India, launched on 2003-09-27 from Guiana Space Centre, Kourou on the e-Bird launch. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,586 km and 35,688 km with an inclination of 9.7°. It travels at approximately 11,089 km/h (3.08 km/s), completing one full orbit every 23 hours 48 minutes — that’s roughly 1.01 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks INSAT 3E in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INSAT 3E occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 9.7°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of INSAT 3E’s average altitude, there are currently 7 active payloads and 24 tracked debris or rocket body fragments. India operates approximately 108 active satellites in total.
❓ Frequently Asked Questions
INSAT 3E orbits at approximately 35,637 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,089 km/h — it just keeps pace with the ground below. With an inclination of 9.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INSAT 3E is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27951. You can track INSAT 3E in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INSAT 3E was launched on 2003-09-27 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks INSAT 3E (NORAD ID 27951) 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.
INSAT 3E travels at approximately 11,089 km/h (6,891 mph) — roughly 3.08 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.