INSAT 2R (ARABSAT 1C)
NORAD 21894
Payload
GEO
1992-010B
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🛰️ Orbital Parameters
Perigee
36121 km
Apogee
36356 km
Inclination
14.3°
Period
1459.2 min
Mean Motion
0.98682699 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,239 km
Orbital Velocity11,011 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0028
Semi-Major Axis42,610 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 Arabsat (India)
Launch Date
1992-02-26
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1992-010B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 2R (ARABSAT 1C) is an active satellite operated by Arabsat (India), launched on 1992-02-26 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 36,121 km and 36,356 km with an inclination of 14.3°. It travels at approximately 11,011 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 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 2R (ARABSAT 1C) 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 2R (ARABSAT 1C) 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 14.3°, 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 2R (ARABSAT 1C)’s average altitude, there are currently 69 active payloads and 13 tracked debris or rocket body fragments. India operates approximately 108 active satellites in total.
❓ Frequently Asked Questions
INSAT 2R (ARABSAT 1C) orbits at approximately 36,239 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 11,011 km/h — it just keeps pace with the ground below. With an inclination of 14.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INSAT 2R (ARABSAT 1C) is operated by Arabsat (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21894. You can track INSAT 2R (ARABSAT 1C) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INSAT 2R (ARABSAT 1C) was launched on 1992-02-26 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 2R (ARABSAT 1C) (NORAD ID 21894) 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 2R (ARABSAT 1C) travels at approximately 11,011 km/h (6,842 mph) — roughly 3.06 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.