THURAYA 4, 62483
Orbit data source: Space-Track
THURAYA 4, 62483 is an Emirian payload satellite in GEO that was launched on Sat, 04 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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62483 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / UAERelated business
None
Manufacturer
ADST/ADSUK
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR NEO, PPS-5000
Mass
5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 22.5 m
Radar Cross Section
58.239 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 THURAYA 4
1 62483U 25001A 25341.93358530 .00000142 00000-0 00000-0 0 9999
2 62483 0.0198 50.1035 0000192 227.1304 180.1085 1.00272649 2262Epoch: 2025-12-07T22:24Z
TLE epoch observation values (Epoch: 2025-12-07T22:24:21.769Z)
Latitude
0.0274°
Longitude
44.30531°
Altitude
35,786.652 km
Speed
3.075 km/s
True Right ascension
06h 29m 20s
True Declination
0° 01' 39"
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
07:02:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,788.233 km
Perigee altitude
35,786.614 km
Semi-major axis
42,165.56 km
Eccentricity
0.00002
Inclination
0.0198°
RAAN
50.1035°
Arg. of periapsis
227.1304°
True anomaly
180.1085°
Mean anomaly
180.1085°
Eccentric anomaly
180.1085°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #1 in the year 2025 (2025-01-04 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.THURAYA 4 Visibility
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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. |
|---|---|---|---|---|---|---|---|
| THURAYA 4 is likely not visible in the next few days. |
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62483 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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