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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
Last TLE update
1 day ago
Origin
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 (6 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, 40 m
Radar Cross Section
58.239 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago
0 THURAYA 4
1 62483U 25001A   25190.94191789  .00000152  00000-0  00000-0 0  9994
2 62483   0.0182  31.5037 0000230 111.8828 168.1237  1.00273639   749
Epoch: 2025-07-09T22:36Z
TLE epoch observation values (Epoch: 2025-07-09T22:36:21.705Z)
Latitude
-0.04427°
Longitude
44.30783°
Altitude
35,786.523 km
Speed
3.075 km/s
True Right ascension
20h 46m 03s
True Declination
0° 02' 39"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
0.04433°
Longitude
-164.14735°
Altitude
35,784.634 km
Speed
3.075 km/s
Apparent Right ascension
07h 04m 31s
Apparent Declination
-4° 58' 08"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:54:29
Azimuth
42.567° NE
Elevation
-47.173°
Doppler factor
1
Orbital elements
Apogee altitude
35,788.115 km
Perigee altitude
35,786.176 km
Semi-major axis
42,165.283 km
Eccentricity
0.00002
Inclination
0.0182°
RAAN
31.5037°
Arg. of periapsis
111.8828°
True anomaly
Unknown
Mean anomaly
168.1237°
Eccentric anomaly
Unknown
Mean motion
0.25067 °/min
Orbital period
1,436.12 mins
BSTAR
0
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62483 neighbors
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

THURAYA 4 Visibility

Observer location: undefined°, undefined°

THURAYA 4 is likely not visible in the next few days
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