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Home Library Satellite Directory EUTE 28B (EUTE W2M)

EUTE 28B (EUTE W2M)

NORAD 33460 Payload GEO 2008-065B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36207 km
Apogee
36225 km
Inclination
5.3°
Period
1458.1 min
Mean Motion
0.98760468 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,216 km
Orbital Velocity11,014 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,587 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
EUTELSAT S.A. (Eutelsat)
Launch Date
2008-12-20
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2008-065B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 28B (EUTE W2M) is an active satellite operated by EUTELSAT S.A. (Eutelsat), launched on 2008-12-20 from Guiana Space Centre, Kourou. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 36,207 km and 36,225 km with an inclination of 5.3°. It travels at approximately 11,014 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 28B (EUTE W2M) 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 28B (EUTE W2M) 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 5.3°, 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 28B (EUTE W2M)’s average altitude, there are currently 84 active payloads and 18 tracked debris or rocket body fragments. Eutelsat operates approximately 62 active satellites in total, of which 8 share a similar altitude band with EUTE 28B (EUTE W2M).
❓ Frequently Asked Questions
EUTE 28B (EUTE W2M) orbits at approximately 36,216 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 11,014 km/h — it just keeps pace with the ground below. With an inclination of 5.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE 28B (EUTE W2M) is operated by EUTELSAT S.A. (Eutelsat). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33460. You can track EUTE 28B (EUTE W2M) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE 28B (EUTE W2M) was launched on 2008-12-20 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 28B (EUTE W2M) (NORAD ID 33460) 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 28B (EUTE W2M) travels at approximately 11,014 km/h (6,844 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.