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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39419 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / UAERelated business
Manufacturer
SatRec Initiative
Mission
Operational Civil Imaging
Bus & Motor
SI-300, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 3 Pan, 1.5 m
Radar Cross Section
2.520 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 DUBAISAT 2
1 39419U 13066D 25300.93084414 .00006915 00000-0 45585-3 0 9996
2 39419 97.4439 292.7769 0013526 107.7313 252.5393 15.07720022651361Epoch: 2025-10-27T22:20Z
TLE epoch observation values (Epoch: 2025-10-27T22:20:24.933Z)
Latitude
-0.00002°
Longitude
-78.8526°
Altitude
549.063 km
Speed
7.586 km/s
True Right ascension
19h 31m 06s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:20:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.51 km
Perigee altitude
530.795 km
Semi-major axis
6,918.29 km
Eccentricity
0.00135
Inclination
97.4439°
RAAN
292.7769°
Arg. of periapsis
107.7313°
True anomaly
252.39152°
Mean anomaly
252.5393°
Eccentric anomaly
252.4654°
Mean motion
3.77177 °/min
Orbital period
95.45 mins
BSTAR
0.00045585
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Other satellites on launch #66 in the year 2013 (2013-11-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DUBAISAT 2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-28 11:39:31.052Z | 44.925° NE | 2025-10-28 11:42:31.052Z | 99.601° ESE | 20.522° | 2025-10-28 11:44:31.052Z | 137.769° SSE |
| 4 mins | 2025-10-28 13:15:31.052Z | 320.72° NNW | 2025-10-28 13:16:31.052Z | 298.596° NW | 21.686° | 2025-10-28 13:19:31.052Z | 240.372° WSW |
| 6 mins | 2025-10-28 23:57:31.052Z | 191.651° SSW | 2025-10-28 23:59:31.052Z | 234.861° WSW | 35.875° | 2025-10-29 00:03:31.052Z | 335.881° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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