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AMC-1 (GE-1)

NORAD 24315 Payload GEO 1996-054A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35979 km
Apogee
36029 km
Inclination
9.1°
Period
1447.2 min
Mean Motion
0.99502372 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,004 km
Orbital Velocity11,041 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0006
Semi-Major Axis42,375 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES
Launch Date
1996-09-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1996-054A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AMC-1 (GE-1) is an active satellite operated by SES, launched on 1996-09-08 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 35,979 km and 36,029 km with an inclination of 9.1°. It travels at approximately 11,041 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 AMC-1 (GE-1) 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-1 (GE-1) 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 9.1°, 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-1 (GE-1)’s average altitude, there are currently 60 active payloads and 30 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 3 share a similar altitude band with AMC-1 (GE-1).
❓ Frequently Asked Questions
AMC-1 (GE-1) orbits at approximately 36,004 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 11,041 km/h — it just keeps pace with the ground below. With an inclination of 9.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AMC-1 (GE-1) is operated by SES. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24315. You can track AMC-1 (GE-1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AMC-1 (GE-1) was launched on 1996-09-08 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 AMC-1 (GE-1) (NORAD ID 24315) 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-1 (GE-1) travels at approximately 11,041 km/h (6,861 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.