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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 (10 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: 20 hours ago

TLE from 20 hours ago
0 THURAYA 4
1 62483U 25001A   25311.11314243  .00000146  00000-0  00000-0 0  9993
2 62483   0.0082 332.5957 0000393 306.6179 212.4499  1.00273788  1958
Epoch: 2025-11-07T02:42Z
TLE epoch observation values (Epoch: 2025-11-07T02:42:55.505Z)
Latitude
-0.00408°
Longitude
44.33469°
Altitude
35,786.917 km
Speed
3.075 km/s
True Right ascension
08h 46m 30s
True Declination
0° 00' 15"
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
19:04:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,788.761 km
Perigee altitude
35,785.447 km
Semi-major axis
42,165.241 km
Eccentricity
0.00004
Inclination
0.0082°
RAAN
332.5957°
Arg. of periapsis
306.6179°
True anomaly
212.44748°
Mean anomaly
212.4499°
Eccentric anomaly
212.44869°
Mean motion
0.25068 °/min
Orbital period
1,436.12 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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