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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
7 hours 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 7 hours ago
0 THURAYA 4
1 62483U 25001A   25186.60580610  .00000155  00000-0  00000-0 0  9990
2 62483   0.0235  35.0014 0000272  91.9739  59.2500  1.00272951   702
Epoch: 2025-07-05T14:32Z
TLE epoch observation values (Epoch: 2025-07-05T14:32:21.647Z)
Latitude
0.01575°
Longitude
44.29895°
Altitude
35,785.173 km
Speed
3.075 km/s
True Right ascension
12h 24m 55s
True Declination
0° 00' 57"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-0.04461°
Longitude
155.5592°
Altitude
35,786.859 km
Speed
3.075 km/s
Apparent Right ascension
20h 02m 16s
Apparent Declination
-5° 02' 56"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
09:52:17
Azimuth
42.652° NE
Elevation
-47.232°
Doppler factor
1
Orbital elements
Apogee altitude
35,788.485 km
Perigee altitude
35,786.192 km
Semi-major axis
42,165.475 km
Eccentricity
0.00003
Inclination
0.0235°
RAAN
35.0014°
Arg. of periapsis
91.9739°
True anomaly
Unknown
Mean anomaly
59.25°
Eccentric anomaly
Unknown
Mean motion
0.25067 °/min
Orbital period
1,436.13 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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