INMARSAT 2-F1
NORAD 20918
Payload
GEO
1990-093A
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GEO · NORAD 20918
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
36147 km
Apogee
36219 km
Inclination
13.0°
Period
1456.4 min
Mean Motion
0.98874507 rev/day
TLE Epoch
2026-06-19 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,183 km
Orbital Velocity11,018 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0008
Semi-Major Axis42,554 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
IM
Launch Date
1990-10-30
Launch Site
Cape Canaveral, Florida
Int'l Designator
1990-093A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INMARSAT 2-F1 is an active satellite operated by IM, launched on 1990-10-30 from Cape Canaveral, Florida. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,147 km and 36,219 km with an inclination of 13.0°. It travels at approximately 11,018 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 INMARSAT 2-F1 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-F1 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 13.0°, 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-F1’s average altitude, there are currently 137 active payloads and 12 tracked debris or rocket body fragments. IM operates approximately 20 active satellites in total, of which 2 share a similar altitude band with INMARSAT 2-F1.
❓ Frequently Asked Questions
INMARSAT 2-F1 orbits at approximately 36,183 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 11,018 km/h — it just keeps pace with the ground below. With an inclination of 13.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INMARSAT 2-F1 is operated by IM. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20918. You can track INMARSAT 2-F1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INMARSAT 2-F1 was launched on 1990-10-30 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 INMARSAT 2-F1 (NORAD ID 20918) 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-F1 travels at approximately 11,018 km/h (6,846 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.