Showing default

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 (8 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, 20.0 m
Radar Cross Section
58.239 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 THURAYA 4
1 62483U 25001A   25258.23650891  .00000124  00000-0  00000-0 0  9994
2 62483   0.0184 133.9525 0000493  92.3555 257.5976  1.00271904  1423
Epoch: 2025-09-15T05:40Z
TLE epoch observation values (Epoch: 2025-09-15T05:40:34.369Z)
Latitude
-0.01119°
Longitude
44.31033°
Altitude
35,786.492 km
Speed
3.075 km/s
True Right ascension
08h 15m 35s
True Declination
0° 00' 40"
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
21:51:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.711 km
Perigee altitude
35,785.553 km
Semi-major axis
42,165.769 km
Eccentricity
0.00005
Inclination
0.0184°
RAAN
133.9525°
Arg. of periapsis
92.3555°
True anomaly
257.59208°
Mean anomaly
257.5976°
Eccentric anomaly
257.59484°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

Documentation

Showing up to 5 results
|