INMARSAT 3-F4
NORAD 24819
Payload
GEO
1997-027A
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GEO · NORAD 24819
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35960 km
Apogee
36051 km
Inclination
11.5°
Period
1447.3 min
Mean Motion
0.99497729 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,006 km
Orbital Velocity11,041 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0011
Semi-Major Axis42,377 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
IM
Launch Date
1997-06-03
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1997-027A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INMARSAT 3-F4 is an active satellite operated by IM, launched on 1997-06-03 from Guiana Space Centre, Kourou. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,960 km and 36,051 km with an inclination of 11.5°. It travels at approximately 11,041 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — 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 3-F4 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 3-F4 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 11.5°, 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 3-F4’s average altitude, there are currently 62 active payloads and 30 tracked debris or rocket body fragments. IM operates approximately 20 active satellites in total.
❓ Frequently Asked Questions
INMARSAT 3-F4 orbits at approximately 36,006 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 11,041 km/h — it just keeps pace with the ground below. With an inclination of 11.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INMARSAT 3-F4 is operated by IM. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24819. You can track INMARSAT 3-F4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INMARSAT 3-F4 was launched on 1997-06-03 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 3-F4 (NORAD ID 24819) 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 3-F4 travels at approximately 11,041 km/h (6,861 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.