GSAT 2
NORAD 27807
Payload
GEO
2003-018A
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GEO · NORAD 27807
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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
35856 km
Apogee
35957 km
Inclination
11.2°
Period
1442.2 min
Mean Motion
0.99847070 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,907 km
Orbital Velocity11,054 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0012
Semi-Major Axis42,278 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2003-05-08
Launch Site
SRI
Int'l Designator
2003-018A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GSAT 2 is an active satellite operated by India, launched on 2003-05-08 from SRI. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,856 km and 35,957 km with an inclination of 11.2°. It travels at approximately 11,054 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 2 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 2 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 11.2°, 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 2’s average altitude, there are currently 62 active payloads and 20 tracked debris or rocket body fragments. India operates approximately 108 active satellites in total, of which 4 share a similar altitude band with GSAT 2.
🔗 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 2 orbits at approximately 35,907 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 11,054 km/h — it just keeps pace with the ground below. With an inclination of 11.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
GSAT 2 is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27807. You can track GSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GSAT 2 was launched on 2003-05-08 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks GSAT 2 (NORAD ID 27807) 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 2 travels at approximately 11,054 km/h (6,869 mph) — roughly 3.07 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.