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GSAT 9

NORAD 42695 Payload GEO 2017-024A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35776 km
Apogee
35799 km
Inclination
0.0°
Period
1436.2 min
Mean Motion
1.00276895 rev/day
TLE Epoch
2026-09-17 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,788 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,159 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 South Asian Association for Regional Cooperation (India)
Launch Date
2017-05-05
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2017-024A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GSAT 9 is an active satellite operated by South Asian Association for Regional Cooperation (India), launched on 2017-05-05 from Satish Dhawan Space Centre, India on the GSAT-9 launch. It orbits in Geostationary Orbit (GEO) at altitudes between 35,776 km and 35,799 km with an inclination of 0.0°. It travels at approximately 11,070 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 9 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 9 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. Within ±50 km of GSAT 9’s average altitude, there are currently 737 active payloads and 50 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. India operates approximately 109 active satellites in total, of which 36 share a similar altitude band with GSAT 9.
🔗 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 9 orbits at approximately 35,788 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 11,070 km/h — it just keeps pace with the ground below. Learn more about geostationary orbits.
GSAT 9 is operated by South Asian Association for Regional Cooperation (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 42695. You can track GSAT 9 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GSAT 9 was launched on 2017-05-05 from Satish Dhawan Space Centre, India, India’s primary launch facility on a barrier island off the coast of Andhra Pradesh. View the full satellite launch log.
Yes — Orbital Radar tracks GSAT 9 (NORAD ID 42695) 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 9 travels at approximately 11,070 km/h (6,878 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.