EUTE 10A (EUTE W2A)
NORAD 34710
Payload
GEO
2009-016A
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GEO · NORAD 34710
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
36363 km
Apogee
36442 km
Inclination
3.0°
Period
1467.7 min
Mean Motion
0.98113761 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,403 km
Orbital Velocity10,990 km/h
Velocity3.05 km/s
Orbital Period24.5 hours
Orbits / Day0.98
Eccentricity0.0009
Semi-Major Axis42,774 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
EUTELSAT S.A. (Eutelsat)
Launch Date
2009-04-03
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2009-016A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 10A (EUTE W2A) is an active satellite operated by EUTELSAT S.A. (Eutelsat), launched on 2009-04-03 from Baikonur, Kazakhstan. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 36,363 km and 36,442 km with an inclination of 3.0°. It travels at approximately 10,990 km/h (3.05 km/s), completing one full orbit every 24.5 hours — that’s roughly 0.98 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 10A (EUTE W2A) 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 10A (EUTE W2A) 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 3.0°, 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 10A (EUTE W2A)’s average altitude, there are currently 22 active payloads and 20 tracked debris or rocket body fragments. Eutelsat operates approximately 62 active satellites in total, of which 5 share a similar altitude band with EUTE 10A (EUTE W2A).
❓ Frequently Asked Questions
EUTE 10A (EUTE W2A) orbits at approximately 36,403 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 10,990 km/h — it just keeps pace with the ground below. With an inclination of 3.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE 10A (EUTE W2A) is operated by EUTELSAT S.A. (Eutelsat). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 34710. You can track EUTE 10A (EUTE W2A) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE 10A (EUTE W2A) was launched on 2009-04-03 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 EUTE 10A (EUTE W2A) (NORAD ID 34710) 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 10A (EUTE W2A) travels at approximately 10,990 km/h (6,829 mph) — roughly 3.05 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.