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AMC-2 (GE-2)

NORAD 24713 Payload GEO 1997-002A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36000 km
Apogee
36025 km
Inclination
10.8°
Period
1447.7 min
Mean Motion
0.99471027 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,013 km
Orbital Velocity11,040 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0003
Semi-Major Axis42,384 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES
Launch Date
1997-01-30
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1997-002A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AMC-2 (GE-2) is an active satellite operated by SES, launched on 1997-01-30 from Guiana Space Centre, Kourou. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,000 km and 36,025 km with an inclination of 10.8°. It travels at approximately 11,040 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — 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-2 (GE-2) 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-2 (GE-2) 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 10.8°, 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-2 (GE-2)’s average altitude, there are currently 61 active payloads and 30 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 4 share a similar altitude band with AMC-2 (GE-2).
❓ Frequently Asked Questions
AMC-2 (GE-2) orbits at approximately 36,013 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 11,040 km/h — it just keeps pace with the ground below. With an inclination of 10.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AMC-2 (GE-2) is operated by SES. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24713. You can track AMC-2 (GE-2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AMC-2 (GE-2) was launched on 1997-01-30 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 AMC-2 (GE-2) (NORAD ID 24713) 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-2 (GE-2) travels at approximately 11,040 km/h (6,860 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.