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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: 3 hours ago

TLE from 3 hours ago
0 DUBAISAT 2
1 39419U 13066D   26037.89226309  .00005012  00000-0  32016-3 0  9992
2 39419  97.4506  31.6074 0013286 116.0193 244.2406 15.09014350666739
Epoch: 2026-02-06T21:24Z
TLE epoch observation values (Epoch: 2026-02-06T21:24:51.530Z)
Latitude
-0.00003°
Longitude
-66.63092°
Altitude
546.29 km
Speed
7.587 km/s
True Right ascension
02h 06m 25s
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
02:42:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.379 km
Perigee altitude
527.007 km
Semi-major axis
6,914.33 km
Eccentricity
0.00133
Inclination
97.4506°
RAAN
31.6074°
Arg. of periapsis
116.0193°
True anomaly
244.10358°
Mean anomaly
244.2406°
Eccentric anomaly
244.17208°
Mean motion
3.77501 °/min
Orbital period
95.36 mins
BSTAR
0.00032016
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