EUTE 172A (GE 23)
NORAD 28924
Payload
GEO
2005-052A
● Active
CONNECTING…
GEO · NORAD 28924
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
35760 km
Apogee
35813 km
Inclination
4.2°
Period
1436.1 min
Mean Motion
1.00271820 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0006
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
EUTELSAT S.A. (Eutelsat)
Launch Date
2005-12-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2005-052A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 172A (GE 23) is an active satellite operated by EUTELSAT S.A. (Eutelsat), launched on 2005-12-29 from Baikonur, Kazakhstan. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,760 km and 35,813 km with an inclination of 4.2°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 172A (GE 23) 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 172A (GE 23) 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 4.2°, 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 172A (GE 23)’s average altitude, there are currently 713 active payloads and 58 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Eutelsat operates approximately 62 active satellites in total, of which 28 share a similar altitude band with EUTE 172A (GE 23).
❓ Frequently Asked Questions
EUTE 172A (GE 23) orbits at approximately 35,787 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 4.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE 172A (GE 23) is operated by EUTELSAT S.A. (Eutelsat). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28924. You can track EUTE 172A (GE 23) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE 172A (GE 23) was launched on 2005-12-29 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 172A (GE 23) (NORAD ID 28924) 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 172A (GE 23) travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 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.