DUBAISAT 2
NORAD 39419
Payload
LEO
2013-066D
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LEO · NORAD 39419
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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
525 km
Apogee
543 km
Inclination
97.5°
Period
95.3 min
Mean Motion
15.10747069 rev/day
TLE Epoch
2026-09-17 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude534 km
Orbital Velocity27,352 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.11
Eccentricity0.0013
Semi-Major Axis6,905 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇦🇪 Emirates Institution for Advanced Science & Technology (EIAST) (UAE)
Launch Date
2013-11-21
Launch Site
Yasny / Dombarovsky, Russia
Int'l Designator
2013-066D
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DUBAISAT 2 is an active satellite operated by Emirates Institution for Advanced Science & Technology (EIAST) (UAE), launched on 2013-11-21 from Yasny / Dombarovsky, Russia on the Dnepr Rideshare 8 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 525 km and 543 km with an inclination of 97.5°. It travels at approximately 27,352 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.11 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 ~3–10 years. Orbital Radar tracks DUBAISAT 2 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 2 orbits at an average altitude of 534 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 2’s average altitude, there are currently 1,775 active payloads and 338 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 9.5% of all active satellites. With an inclination of 97.5°, DUBAISAT 2 passes over latitudes between 97.5°N and 97.5°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 11 share a similar altitude band with DUBAISAT 2.
❓ Frequently Asked Questions
DUBAISAT 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 534 km altitude. Its 97.5° 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 95 minutes, travelling at 27,352 km/h.
DUBAISAT 2 is operated by Emirates Institution for Advanced Science & Technology (EIAST) (UAE). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39419. You can track DUBAISAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DUBAISAT 2 was launched on 2013-11-21 from Yasny / Dombarovsky, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks DUBAISAT 2 (NORAD ID 39419) 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 2 travels at approximately 27,352 km/h (16,996 mph) — roughly 7.60 km/s. It completes 15.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.