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AMC-14

NORAD 32708 Payload GEO 2008-011A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35571 km
Apogee
35955 km
Inclination
24.0°
Period
1434.9 min
Mean Motion
1.00355279 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,763 km
Orbital Velocity11,073 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0046
Semi-Major Axis42,134 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2008-03-14
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2008-011A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AMC-14 is an active satellite operated by United States, launched on 2008-03-14 from Baikonur, Kazakhstan. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,571 km and 35,955 km with an inclination of 24.0°. It travels at approximately 11,073 km/h (3.08 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-14 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-14 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 24.0°, 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 AMC-14’s average altitude, there are currently 694 active payloads and 53 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 12,360 active satellites in total, of which 142 share a similar altitude band with AMC-14.
❓ Frequently Asked Questions
AMC-14 orbits at approximately 35,763 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 11,073 km/h — it just keeps pace with the ground below. With an inclination of 24.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AMC-14 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 32708. You can track AMC-14 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AMC-14 was launched on 2008-03-14 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-14 (NORAD ID 32708) 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-14 travels at approximately 11,073 km/h (6,880 mph) — roughly 3.08 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.