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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.

Not visible in the next 10 days
Identifier
62483, 2025-001A
Orbit
GEO
Country
Flag of AEAE / UAE
Related 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)
2025-01-04 (11 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 22.5 m
Radar Cross Section
58.239 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 THURAYA 4
1 62483U 25001A   25346.21379207  .00000149  00000-0  00000-0 0  9996
2 62483   0.0205  57.2199 0000067 304.5489 200.6650  1.00273278  2305
Epoch: 2025-12-12T05:07Z
TLE epoch observation values (Epoch: 2025-12-12T05:07:51.634Z)
Latitude
-0.00027°
Longitude
44.30442°
Altitude
35,785.93 km
Speed
3.075 km/s
True Right ascension
13h 29m 42s
True Declination
0° 00' 01"
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
22:42:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,787.529 km
Perigee altitude
35,786.964 km
Semi-major axis
42,165.384 km
Eccentricity
0.00001
Inclination
0.0205°
RAAN
57.2199°
Arg. of periapsis
304.5489°
True anomaly
200.66473°
Mean anomaly
200.665°
Eccentric anomaly
200.66486°
Mean motion
0.25067 °/min
Orbital period
1,436.13 mins
BSTAR
0
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

Documentation

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