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Home Library Satellite Directory EUTE 1-F4 (ECS 4)

EUTE 1-F4 (ECS 4)

NORAD 18351 Payload GEO 1987-078B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36186 km
Apogee
36286 km
Inclination
13.9°
Period
1459.1 min
Mean Motion
0.98691194 rev/day
TLE Epoch
2026-05-08 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,236 km
Orbital Velocity11,011 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0012
Semi-Major Axis42,607 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Eutelsat
Launch Date
1987-09-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1987-078B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 1-F4 (ECS 4) is an active satellite operated by Eutelsat, launched on 1987-09-16 from Guiana Space Centre, Kourou. With over 39 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,186 km and 36,286 km with an inclination of 13.9°. It travels at approximately 11,011 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 EUTE 1-F4 (ECS 4) 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 1-F4 (ECS 4) occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 13.9°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
❓ Frequently Asked Questions
EUTE 1-F4 (ECS 4) orbits at approximately 36,236 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 11,011 km/h — it just keeps pace with the ground below. With an inclination of 13.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
EUTE 1-F4 (ECS 4) is operated by Eutelsat. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 18351. You can track EUTE 1-F4 (ECS 4) in real time on Orbital Radar’s live tracker.
EUTE 1-F4 (ECS 4) was launched on 1987-09-16 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.
Yes — Orbital Radar tracks EUTE 1-F4 (ECS 4) (NORAD ID 18351) 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.
EUTE 1-F4 (ECS 4) travels at approximately 11,011 km/h (6,842 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.
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