EUTE 2-F2
NORAD 21056
Payload
GEO
1991-003B
● Active
CONNECTING…
GEO · NORAD 21056
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36157 km
Apogee
36170 km
Inclination
14.9°
Period
1455.4 min
Mean Motion
0.98941984 rev/day
TLE Epoch
2026-05-08 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,164 km
Orbital Velocity11,020 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,535 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Eutelsat
Launch Date
1991-01-15
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1991-003B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 2-F2 is an active satellite operated by Eutelsat, launched on 1991-01-15 from Guiana Space Centre, Kourou. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,157 km and 36,170 km with an inclination of 14.9°. It travels at approximately 11,020 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 2-F2 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-F2 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 14.9°, 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 2-F2 orbits at approximately 36,164 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 11,020 km/h — it just keeps pace with the ground below. With an inclination of 14.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
EUTE 2-F2 is operated by Eutelsat. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21056. You can track EUTE 2-F2 in real time on Orbital Radar’s live tracker.
EUTE 2-F2 was launched on 1991-01-15 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 2-F2 (NORAD ID 21056) 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 2-F2 travels at approximately 11,020 km/h (6,848 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.