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INMARSAT 4-F3

NORAD 33278 Payload GEO 2008-039A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35775 km
Apogee
35799 km
Inclination
4.3°
Period
1436.1 min
Mean Motion
1.00271383 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
INMARSAT, Ltd. (IM)
Launch Date
2008-08-18
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2008-039A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INMARSAT 4-F3 is an active satellite operated by INMARSAT, Ltd. (IM), launched on 2008-08-18 from Baikonur, Kazakhstan. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,775 km and 35,799 km with an inclination of 4.3°. It travels at approximately 11,070 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 INMARSAT 4-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 4-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 4.3°, 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 INMARSAT 4-F3’s average altitude, there are currently 713 active payloads and 58 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. IM operates approximately 20 active satellites in total, of which 11 share a similar altitude band with INMARSAT 4-F3.
❓ Frequently Asked Questions
INMARSAT 4-F3 orbits at approximately 35,787 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 4.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INMARSAT 4-F3 is operated by INMARSAT, Ltd. (IM). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33278. You can track INMARSAT 4-F3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INMARSAT 4-F3 was launched on 2008-08-18 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks INMARSAT 4-F3 (NORAD ID 33278) 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 4-F3 travels at approximately 11,070 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.