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EUTE 48A (HB2)

NORAD 24665 Payload GEO 1996-067A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36302 km
Apogee
36347 km
Inclination
12.0°
Period
1463.7 min
Mean Motion
0.98383351 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,325 km
Orbital Velocity11,000 km/h
Velocity3.06 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0005
Semi-Major Axis42,696 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Eutelsat
Launch Date
1996-11-21
Launch Site
Cape Canaveral, Florida
Int'l Designator
1996-067A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 48A (HB2) is an active satellite operated by Eutelsat, launched on 1996-11-21 from Cape Canaveral, Florida. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,302 km and 36,347 km with an inclination of 12.0°. It travels at approximately 11,000 km/h (3.06 km/s), completing one full orbit every 24.4 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 48A (HB2) 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 48A (HB2) 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 12.0°, 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 48A (HB2)’s average altitude, there are currently 46 active payloads and 8 tracked debris or rocket body fragments. Eutelsat operates approximately 62 active satellites in total, of which 9 share a similar altitude band with EUTE 48A (HB2).
❓ Frequently Asked Questions
EUTE 48A (HB2) orbits at approximately 36,325 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 11,000 km/h — it just keeps pace with the ground below. With an inclination of 12.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE 48A (HB2) is operated by Eutelsat. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24665. You can track EUTE 48A (HB2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE 48A (HB2) was launched on 1996-11-21 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks EUTE 48A (HB2) (NORAD ID 24665) 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 48A (HB2) travels at approximately 11,000 km/h (6,835 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.