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INMARSAT 2-F3

NORAD 21814 Payload GEO 1991-084B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36946 km
Apogee
37074 km
Inclination
14.1°
Period
1499.0 min
Mean Motion
0.96061818 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,010 km
Orbital Velocity10,912 km/h
Velocity3.03 km/s
Orbital Period25.0 hours
Orbits / Day0.96
Eccentricity0.0015
Semi-Major Axis43,381 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
IM
Launch Date
1991-12-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1991-084B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INMARSAT 2-F3 is an active satellite operated by IM, launched on 1991-12-16 from Guiana Space Centre, Kourou. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,946 km and 37,074 km with an inclination of 14.1°. It travels at approximately 10,912 km/h (3.03 km/s), completing one full orbit every 25.0 hours — that’s roughly 0.96 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 INMARSAT 2-F3 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INMARSAT 2-F3 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 14.1°, 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 INMARSAT 2-F3’s average altitude, there are currently 6 active payloads and 2 tracked debris or rocket body fragments. IM operates approximately 20 active satellites in total.
❓ Frequently Asked Questions
INMARSAT 2-F3 orbits at approximately 37,010 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 10,912 km/h — it just keeps pace with the ground below. With an inclination of 14.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INMARSAT 2-F3 is operated by IM. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21814. You can track INMARSAT 2-F3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INMARSAT 2-F3 was launched on 1991-12-16 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 INMARSAT 2-F3 (NORAD ID 21814) 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.
INMARSAT 2-F3 travels at approximately 10,912 km/h (6,781 mph) — roughly 3.03 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.