GSAT 3 (EDUSAT)
NORAD 28417
Payload
GEO
2004-036A
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GEO · NORAD 28417
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Altitude (km)
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Speed (km/s)
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Latitude
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🛰️ Orbital Parameters
Perigee
36058 km
Apogee
36082 km
Inclination
11.4°
Period
1450.6 min
Mean Motion
0.99270729 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,070 km
Orbital Velocity11,033 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0003
Semi-Major Axis42,441 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2004-09-20
Launch Site
SRI
Int'l Designator
2004-036A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GSAT 3 (EDUSAT) is an active satellite operated by India, launched on 2004-09-20 from SRI. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,058 km and 36,082 km with an inclination of 11.4°. It travels at approximately 11,033 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 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 GSAT 3 (EDUSAT) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GSAT 3 (EDUSAT) 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 11.4°, 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 GSAT 3 (EDUSAT)’s average altitude, there are currently 128 active payloads and 18 tracked debris or rocket body fragments. India operates approximately 108 active satellites in total, of which 4 share a similar altitude band with GSAT 3 (EDUSAT).
🔗 Galileo Navigation Constellation
This satellite is part of Galileo, the European Union's global navigation satellite system. Galileo provides high-accuracy positioning independent of GPS, GLONASS and BeiDou. The constellation operates at approximately 23,222 km altitude in three orbital planes with an inclination of 56°. Galileo offers multiple services including the Open Service (free, metre-level accuracy), High Accuracy Service (centimetre-level) and the Search and Rescue return-link service.
❓ Frequently Asked Questions
GSAT 3 (EDUSAT) orbits at approximately 36,070 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 11,033 km/h — it just keeps pace with the ground below. With an inclination of 11.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
GSAT 3 (EDUSAT) is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28417. You can track GSAT 3 (EDUSAT) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GSAT 3 (EDUSAT) was launched on 2004-09-20 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks GSAT 3 (EDUSAT) (NORAD ID 28417) 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.
GSAT 3 (EDUSAT) travels at approximately 11,033 km/h (6,855 mph) — roughly 3.06 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.