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Home Library Satellite Directory EUTE HOT BIRD 13C (HB 9)

EUTE HOT BIRD 13C (HB 9)

NORAD 33459 Payload GEO 2008-065A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35773 km
Apogee
35801 km
Inclination
3.0°
Period
1436.1 min
Mean Motion
1.00270093 rev/day
TLE Epoch
2026-06-19 21:00:00 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
Eccentricity0.0003
Semi-Major Axis42,158 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
2008-065A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE HOT BIRD 13C (HB 9) 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 35,773 km and 35,801 km with an inclination of 3.0°. 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 HOT BIRD 13C (HB 9) 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 HOT BIRD 13C (HB 9) 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 HOT BIRD 13C (HB 9)’s average altitude, there are currently 713 active payloads and 59 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 HOT BIRD 13C (HB 9).
❓ Frequently Asked Questions
EUTE HOT BIRD 13C (HB 9) 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 3.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE HOT BIRD 13C (HB 9) is operated by EUTELSAT S.A. (Eutelsat). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33459. You can track EUTE HOT BIRD 13C (HB 9) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE HOT BIRD 13C (HB 9) 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 HOT BIRD 13C (HB 9) (NORAD ID 33459) 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 HOT BIRD 13C (HB 9) 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.