DUBAISAT 1
NORAD 35682
Payload
LEO
2009-041B
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LEO · NORAD 35682
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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
637 km
Apogee
653 km
Inclination
98.0°
Period
97.6 min
Mean Motion
14.75125326 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude645 km
Orbital Velocity27,135 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.75
Eccentricity0.0011
Semi-Major Axis7,016 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇦🇪 UAE
Launch Date
2009-07-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2009-041B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DUBAISAT 1 is an active satellite operated by UAE, launched on 2009-07-29 from Baikonur, Kazakhstan. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 637 km and 653 km with an inclination of 98.0°. It travels at approximately 27,135 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.75 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks DUBAISAT 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
DUBAISAT 1 orbits at an average altitude of 645 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of DUBAISAT 1’s average altitude, there are currently 691 active payloads and 986 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0050. With an inclination of 98.0°, DUBAISAT 1 passes over latitudes between 98.0°N and 98.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. UAE operates approximately 22 active satellites in total, of which 2 share a similar altitude band with DUBAISAT 1.
❓ Frequently Asked Questions
DUBAISAT 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 645 km altitude. Its 98.0° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 98 minutes, travelling at 27,135 km/h.
DUBAISAT 1 is operated by UAE. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 35682. You can track DUBAISAT 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DUBAISAT 1 was launched on 2009-07-29 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks DUBAISAT 1 (NORAD ID 35682) 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.
DUBAISAT 1 travels at approximately 27,135 km/h (16,861 mph) — roughly 7.54 km/s. It completes 14.75 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.