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EUTE 2-F4

NORAD 22028 Payload GEO 1992-041B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36093 km
Apogee
36158 km
Inclination
14.7°
Period
1453.5 min
Mean Motion
0.99074409 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,126 km
Orbital Velocity11,025 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0008
Semi-Major Axis42,497 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Eutelsat
Launch Date
1992-07-09
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1992-041B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 2-F4 is an active satellite operated by Eutelsat, launched on 1992-07-09 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 36,093 km and 36,158 km with an inclination of 14.7°. It travels at approximately 11,025 km/h (3.06 km/s), completing one full orbit every 24.2 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 EUTE 2-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
EUTE 2-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 14.7°, 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 EUTE 2-F4’s average altitude, there are currently 192 active payloads and 6 tracked debris or rocket body fragments. Eutelsat operates approximately 62 active satellites in total, of which 5 share a similar altitude band with EUTE 2-F4.
❓ Frequently Asked Questions
EUTE 2-F4 orbits at approximately 36,126 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 11,025 km/h — it just keeps pace with the ground below. With an inclination of 14.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE 2-F4 is operated by Eutelsat. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22028. You can track EUTE 2-F4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE 2-F4 was launched on 1992-07-09 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 EUTE 2-F4 (NORAD ID 22028) 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.
EUTE 2-F4 travels at approximately 11,025 km/h (6,851 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.