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AMOS 2

NORAD 28132 Payload GEO 2003-059A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36026 km
Apogee
36041 km
Inclination
8.5°
Period
1448.7 min
Mean Motion
0.99397640 rev/day
TLE Epoch
2026-06-18 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,034 km
Orbital Velocity11,037 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,405 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇱 Israel
Launch Date
2003-12-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2003-059A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AMOS 2 is an active satellite operated by Israel, launched on 2003-12-27 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 36,026 km and 36,041 km with an inclination of 8.5°. It travels at approximately 11,037 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 AMOS 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
AMOS 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 8.5°, 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 AMOS 2’s average altitude, there are currently 77 active payloads and 28 tracked debris or rocket body fragments. Israel operates approximately 11 active satellites in total, of which 2 share a similar altitude band with AMOS 2.
❓ Frequently Asked Questions
AMOS 2 orbits at approximately 36,034 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 11,037 km/h — it just keeps pace with the ground below. With an inclination of 8.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AMOS 2 is operated by Israel. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28132. You can track AMOS 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AMOS 2 was launched on 2003-12-27 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 AMOS 2 (NORAD ID 28132) 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.
AMOS 2 travels at approximately 11,037 km/h (6,858 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.