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DUBAISAT 2, 39419

Orbit data source: Space-Track

DUBAISAT 2, 39419 is a payload satellite owned by EIAST (AE) in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
39419, 2013-066D
Orbit
SSO
Country
Flag of AEAE / UAE
Related business
Manufacturer
SatRec Initiative
Mission
Operational Civil Imaging
Bus & Motor
SI-300, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
2013-11-21 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Cyl + 3 Pan, 1.5 m
Radar Cross Section
2.520 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 DUBAISAT 2
1 39419U 13066D   26092.25609334  .00009011  00000-0  56348-3 0  9993
2 39419  97.4541  84.4331 0009805 299.4850  60.5401 15.09611701674936
Epoch: 2026-04-02T06:08Z
TLE epoch observation values (Epoch: 2026-04-02T06:08:46.464Z)
Latitude
-0.00001°
Longitude
161.63231°
Altitude
537.13 km
Speed
7.596 km/s
True Right ascension
05h 37m 43s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:06:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.145 km
Perigee altitude
527.59 km
Semi-major axis
6,912.504 km
Eccentricity
0.00098
Inclination
97.4541°
RAAN
84.4331°
Arg. of periapsis
299.485°
True anomaly
60.63799°
Mean anomaly
60.5401°
Eccentric anomaly
60.58904°
Mean motion
3.7765 °/min
Orbital period
95.33 mins
BSTAR
0.00056348
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