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GSAT 6A

NORAD 43241 Payload MEO 2018-027A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
26231 km
Apogee
36111 km
Inclination
3.3°
Period
1206.9 min
Mean Motion
1.19316262 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude31,171 km
Orbital Velocity11,730 km/h
Velocity3.26 km/s
Orbital Period20 hours 7 minutes
Orbits / Day1.19
Eccentricity0.1316
Semi-Major Axis37,542 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2018-03-29
Launch Site
SRI
Int'l Designator
2018-027A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GSAT 6A is an active satellite operated by India, launched on 2018-03-29 from SRI. It orbits in Medium Earth Orbit (MEO) at altitudes between 26,231 km and 36,111 km with an inclination of 3.3°. It travels at approximately 11,730 km/h (3.26 km/s), completing one full orbit every 20 hours 7 minutes — that’s roughly 1.19 orbits per day. Its orbital eccentricity of 0.1316 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks GSAT 6A 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 6A orbits at an average altitude of 31,171 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. With an inclination of 3.3°, GSAT 6A passes over latitudes between 3.3°N and 3.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. India operates approximately 108 active satellites in total.
🔗 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 6A orbits in Medium Earth Orbit (MEO) at altitudes between 26,231 km (perigee) and 36,111 km (apogee), with an average altitude of approximately 31,171 km. It completes one orbit every 20 hours 7 minutes, travelling at approximately 11,730 km/h (7,289 mph).
GSAT 6A is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43241. You can track GSAT 6A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GSAT 6A was launched on 2018-03-29 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks GSAT 6A (NORAD ID 43241) 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 6A travels at approximately 11,730 km/h (7,289 mph) — roughly 3.26 km/s. It completes 1.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.