ARABSAT 1DR (TELSTAR 3A)
NORAD 14234
Payload
GEO
1983-077A
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GEO · NORAD 14234
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35891 km
Apogee
36102 km
Inclination
13.8°
Period
1446.8 min
Mean Motion
0.99527249 rev/day
TLE Epoch
2026-06-18 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,997 km
Orbital Velocity11,042 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0025
Semi-Major Axis42,368 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Arabsat (Saudi Arabia)
Launch Date
1983-07-28
Launch Site
Cape Canaveral, Florida
Int'l Designator
1983-077A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ARABSAT 1DR (TELSTAR 3A) is an active satellite operated by Arabsat (Saudi Arabia), launched on 1983-07-28 from Cape Canaveral, Florida. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,891 km and 36,102 km with an inclination of 13.8°. It travels at approximately 11,042 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 1DR (TELSTAR 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 1DR (TELSTAR 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 13.8°, 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 ARABSAT 1DR (TELSTAR 3A)’s average altitude, there are currently 57 active payloads and 29 tracked debris or rocket body fragments. Saudi Arabia operates approximately 15 active satellites in total, of which 2 share a similar altitude band with ARABSAT 1DR (TELSTAR 3A).
❓ Frequently Asked Questions
ARABSAT 1DR (TELSTAR 3A) orbits at approximately 35,997 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 11,042 km/h — it just keeps pace with the ground below. With an inclination of 13.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ARABSAT 1DR (TELSTAR 3A) is operated by Arabsat (Saudi Arabia). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 14234. You can track ARABSAT 1DR (TELSTAR 3A) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ARABSAT 1DR (TELSTAR 3A) was launched on 1983-07-28 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks ARABSAT 1DR (TELSTAR 3A) (NORAD ID 14234) 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 1DR (TELSTAR 3A) travels at approximately 11,042 km/h (6,861 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.