THURAYA 1
NORAD 26578
Payload
GEO
2000-066A
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GEO · NORAD 26578
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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
36113 km
Apogee
36188 km
Inclination
9.8°
Period
1454.7 min
Mean Motion
0.98987744 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,151 km
Orbital Velocity11,022 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0009
Semi-Major Axis42,522 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇦🇪 UAE
Launch Date
2000-10-21
Launch Site
Sea Launch (ocean platform)
Int'l Designator
2000-066A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
THURAYA 1 is an active satellite operated by UAE, launched on 2000-10-21 from Sea Launch (ocean platform). With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,113 km and 36,188 km with an inclination of 9.8°. It travels at approximately 11,022 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 THURAYA 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
THURAYA 1 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 9.8°, 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 THURAYA 1’s average altitude, there are currently 172 active payloads and 9 tracked debris or rocket body fragments. UAE operates approximately 22 active satellites in total.
❓ Frequently Asked Questions
THURAYA 1 orbits at approximately 36,151 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 11,022 km/h — it just keeps pace with the ground below. With an inclination of 9.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
THURAYA 1 is operated by UAE. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26578. You can track THURAYA 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
THURAYA 1 was launched on 2000-10-21 from Sea Launch (ocean platform). View the full satellite launch log.
Yes — Orbital Radar tracks THURAYA 1 (NORAD ID 26578) 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.
THURAYA 1 travels at approximately 11,022 km/h (6,849 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.