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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62483 intel report (Beta)
THURAYA 4 details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 5 days ago |
| Origin | |
| Manufacturer | ADST/ADSUK |
| Mission | Operational spacecraft |
| Bus & Motor | EUROSTAR NEO, PPS-5000 |
| Mass | 5,000 kg wet, ~5,000 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 5 days ago
0 THURAYA 4
1 62483U 25001A 25031.26288702 -.00000297 00000-0 00000+0 0 9995
2 62483 16.4825 317.3268 7356548 184.3363 161.0669 1.16876655 360Epoch: 2025-01-31T06:18Z
Definitive object data (Epoch: 2025-01-31T06:18:33.438Z)
| Latitude | 0.00009° |
| Longitude | 91.99911° |
| Altitude | 59,277.41 km |
| Speed | 1.293 km/s |
| True Right ascension | 21h 09m 27s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -5.91449° |
| Longitude | 71.03699° |
| Altitude | 44,791.484 km |
| Speed | 2.26 km/s |
| Apparent Right ascension | 19h 41m 21s |
| Apparent Declination | -9° 31' 09" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 06:56:49 |
| Azimuth | 338.921° N |
| Elevation | -58.028° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 59,704.031 km |
| Perigee altitude | 3,686.367 km |
| Semi-major axis | 38,073.336 km |
| Eccentricity | 0.7356548 |
| Inclination | 16.4825° |
| RAAN | 317.3268° |
| Arg. of periapsis | 184.3363° |
| True anomaly | 175.72093° |
| Mean anomaly | 161.0669° |
| Eccentric anomaly | 169.06357° |
| Mean motion | 0.29215 °/min |
| BSTAR | Unknown |
| Orbital period | 1232.23 mins |
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)
| THURAYA 4, 62483 |
| OBJECT B, 62484 |
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. |
|---|---|---|---|---|---|---|---|
| 219 mins | 2025-02-05 16:01:53.995Z | 93.677° ESE | 2025-02-05 18:25:53.995Z | 99.867° ESE | 20.326° | 2025-02-05 19:40:53.995Z | 90.984° ESE |
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