INSAT 1A
NORAD 13129
Payload
GEO
1982-031A
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GEO · NORAD 13129
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🛰️ Orbital Parameters
Perigee
35712 km
Apogee
35833 km
Inclination
7.1°
Period
1435.4 min
Mean Motion
1.00320736 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,773 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0014
Semi-Major Axis42,144 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
1982-04-10
Launch Site
Cape Canaveral, Florida
Int'l Designator
1982-031A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 1A is an active satellite operated by India, launched on 1982-04-10 from Cape Canaveral, Florida. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,712 km and 35,833 km with an inclination of 7.1°. It travels at approximately 11,071 km/h (3.08 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 1A 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 1A 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 7.1°, 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 1A’s average altitude, there are currently 707 active payloads and 57 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 1A.
❓ Frequently Asked Questions
INSAT 1A orbits at approximately 35,773 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 11,071 km/h — it just keeps pace with the ground below. With an inclination of 7.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INSAT 1A is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13129. You can track INSAT 1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INSAT 1A was launched on 1982-04-10 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks INSAT 1A (NORAD ID 13129) 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 1A travels at approximately 11,071 km/h (6,880 mph) — roughly 3.08 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.