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ARABSAT 2A

NORAD 23948 Payload GEO 1996-040A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36068 km
Apogee
36095 km
Inclination
14.3°
Period
1451.2 min
Mean Motion
0.99228464 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,082 km
Orbital Velocity11,031 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0003
Semi-Major Axis42,453 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Arabsat (Saudi Arabia)
Launch Date
1996-07-09
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1996-040A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ARABSAT 2A is an active satellite operated by Arabsat (Saudi Arabia), launched on 1996-07-09 from Guiana Space Centre, Kourou. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,068 km and 36,095 km with an inclination of 14.3°. It travels at approximately 11,031 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 ARABSAT 2A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ARABSAT 2A 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 14.3°, 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 ARABSAT 2A’s average altitude, there are currently 142 active payloads and 12 tracked debris or rocket body fragments. Saudi Arabia operates approximately 15 active satellites in total.
❓ Frequently Asked Questions
ARABSAT 2A orbits at approximately 36,082 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 11,031 km/h — it just keeps pace with the ground below. With an inclination of 14.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ARABSAT 2A is operated by Arabsat (Saudi Arabia). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23948. You can track ARABSAT 2A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ARABSAT 2A was launched on 1996-07-09 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 ARABSAT 2A (NORAD ID 23948) 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.
ARABSAT 2A travels at approximately 11,031 km/h (6,854 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.