AMC-9 (GE-12)
NORAD 27820
Payload
GEO
2003-024A
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GEO · NORAD 27820
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🛰️ Orbital Parameters
Perigee
36060 km
Apogee
36215 km
Inclination
7.9°
Period
1454.0 min
Mean Motion
0.99033964 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,138 km
Orbital Velocity11,024 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0018
Semi-Major Axis42,509 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES
Launch Date
2003-06-06
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2003-024A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AMC-9 (GE-12) is an active satellite operated by SES, launched on 2003-06-06 from Baikonur, Kazakhstan. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,060 km and 36,215 km with an inclination of 7.9°. It travels at approximately 11,024 km/h (3.06 km/s), completing one full orbit every 24.2 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 AMC-9 (GE-12) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AMC-9 (GE-12) 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 7.9°, 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 AMC-9 (GE-12)’s average altitude, there are currently 187 active payloads and 8 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 22 share a similar altitude band with AMC-9 (GE-12).
❓ Frequently Asked Questions
AMC-9 (GE-12) orbits at approximately 36,138 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 11,024 km/h — it just keeps pace with the ground below. With an inclination of 7.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AMC-9 (GE-12) is operated by SES. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27820. You can track AMC-9 (GE-12) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AMC-9 (GE-12) was launched on 2003-06-06 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 AMC-9 (GE-12) (NORAD ID 27820) 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.
AMC-9 (GE-12) travels at approximately 11,024 km/h (6,850 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.