Skip to content
Home Library Satellite Directory ARABSAT 3A

ARABSAT 3A

NORAD 25638 Payload GEO 1999-009A ● Active
CONNECTING… GEO · NORAD 25638
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35794 km
Apogee
35838 km
Inclination
11.9°
Period
1437.6 min
Mean Motion
1.00167389 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,816 km
Orbital Velocity11,066 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0005
Semi-Major Axis42,187 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Arabsat (Saudi Arabia)
Launch Date
1999-02-26
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1999-009A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ARABSAT 3A is an active satellite operated by Arabsat (Saudi Arabia), launched on 1999-02-26 from Guiana Space Centre, Kourou. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,794 km and 35,838 km with an inclination of 11.9°. It travels at approximately 11,066 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 ARABSAT 3A 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 3A 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 11.9°, 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 3A’s average altitude, there are currently 706 active payloads and 67 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Saudi Arabia operates approximately 15 active satellites in total, of which 9 share a similar altitude band with ARABSAT 3A.
❓ Frequently Asked Questions
ARABSAT 3A orbits at approximately 35,816 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 11,066 km/h — it just keeps pace with the ground below. With an inclination of 11.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ARABSAT 3A is operated by Arabsat (Saudi Arabia). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25638. You can track ARABSAT 3A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ARABSAT 3A was launched on 1999-02-26 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 3A (NORAD ID 25638) 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 3A travels at approximately 11,066 km/h (6,876 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.