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THURAYA 4, 62483

Orbit data source: Space-Track

THURAYA 4, 62483 is an Emirian payload satellite in HEO that was launched on Sat, 04 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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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THURAYA 4 details
Identifier
62483, 2025-001A
Orbit
HEO
Last TLE update4 days ago
Origin
Flag of AESP42/THUR (AE / UAE)
ManufacturerADST/ADSUK
MissionOperational spacecraft
Bus & MotorEUROSTAR NEO, PPS-5000
Mass5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
2025-01-04 (3 weeks ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRUnknown
Radar Cross SectionLarge (>1 m²)

Expand to show TLE details & history

TLE from 4 days ago
0 THURAYA 4
1 62483U 25001A   25021.75000000 -.00000297  00000-0  00000-0 0  9992
2 62483  20.3998 318.6966 7658322 181.7701 306.5259  1.26418201    19
Epoch: 2025-01-21T18:00Z
Definitive object data (Epoch: 2025-01-21T18:00:00Z)
Latitude12.24426°
Longitude-37.07219°
Altitude33,072.513 km
Speed3.029 km/s
True Right ascension23h 37m 07s
True Declination12° 13' 53"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude19.4°
Longitude36.35781°
Altitude5,922.679 km
Speed7.334 km/s
Apparent Right ascension05h 39m 55s
Apparent Declination0° 00' 23"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time20:38:42
Azimuth57.032° ENE
Elevation-33.034°
Doppler factor1
Orbital elements
Apogee altitude57,427.179 km
Perigee altitude2,083.115 km
Semi-major axis36,133.284 km
Eccentricity0.7658322
Inclination20.3998°
RAAN318.6966°
Arg. of periapsis181.7701°
True anomaly215.70173°
Mean anomaly306.5259°
Eccentric anomaly262.97624°
Mean motion0.316 °/min
BSTARUnknown
Orbital period1139.25 mins
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

THURAYA 4 Visibility forecast

Observer location: undefined°, undefined

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.
222 mins2025-01-26 15:35:47.613Z188.7° SSW2025-01-26 19:17:47.613Z194.51° SSW30.887°2025-01-26 19:17:47.613Z194.51° SSW
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