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 | 4 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 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)
Latitude | 12.24426° |
Longitude | -37.07219° |
Altitude | 33,072.513 km |
Speed | 3.029 km/s |
True Right ascension | 23h 37m 07s |
True Declination | 12° 13' 53" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 19.4° |
Longitude | 36.35781° |
Altitude | 5,922.679 km |
Speed | 7.334 km/s |
Apparent Right ascension | 05h 39m 55s |
Apparent Declination | 0° 00' 23" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 20:38:42 |
Azimuth | 57.032° ENE |
Elevation | -33.034° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 57,427.179 km |
Perigee altitude | 2,083.115 km |
Semi-major axis | 36,133.284 km |
Eccentricity | 0.7658322 |
Inclination | 20.3998° |
RAAN | 318.6966° |
Arg. of periapsis | 181.7701° |
True anomaly | 215.70173° |
Mean anomaly | 306.5259° |
Eccentric anomaly | 262.97624° |
Mean motion | 0.316 °/min |
BSTAR | Unknown |
Orbital period | 1139.25 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. |
---|---|---|---|---|---|---|---|
222 mins | 2025-01-26 15:35:47.613Z | 188.7° SSW | 2025-01-26 19:17:47.613Z | 194.51° SSW | 30.887° | 2025-01-26 19:17:47.613Z | 194.51° SSW |
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