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INSAT 2A

NORAD 22027 Payload GEO 1992-041A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35760 km
Apogee
35833 km
Inclination
14.5°
Period
1436.6 min
Mean Motion
1.00237318 rev/day
TLE Epoch
2026-06-18 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,797 km
Orbital Velocity11,068 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0009
Semi-Major Axis42,168 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
1992-07-09
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1992-041A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 2A is an active satellite operated by India, launched on 1992-07-09 from Guiana Space Centre, Kourou. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,760 km and 35,833 km with an inclination of 14.5°. It travels at approximately 11,068 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 INSAT 2A 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 2A 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 14.5°, 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 2A’s average altitude, there are currently 714 active payloads and 63 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. India operates approximately 108 active satellites in total, of which 36 share a similar altitude band with INSAT 2A.
❓ Frequently Asked Questions
INSAT 2A orbits at approximately 35,797 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 11,068 km/h — it just keeps pace with the ground below. With an inclination of 14.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INSAT 2A is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22027. You can track INSAT 2A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INSAT 2A was launched on 1992-07-09 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 2A (NORAD ID 22027) 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 2A travels at approximately 11,068 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.