EGYPTSAT A, 44047
Orbit data source: Space-Track
EGYPTSAT A, 44047 is a payload satellite owned by EgSA (EG) in SSO that was launched on Thu, 21 Feb 2019 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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44047 intel report (Beta)
EGYPTSAT A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 hours ago |
| Origin | |
| Manufacturer | Yuzhnoe |
| Mission | Operational Civil Imaging |
| Bus & Motor | EGYPTSAT, Unknown motor |
| Mass | ~1,050 kg wet, ~1,050 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 4 Pan + 1 Ant, 2 m |
| Radar Cross Section | 0.867 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 5 hours ago
0 EGYPTSAT A
1 44047U 19008A 24361.29866193 .00001870 00000-0 30373-3 0 9992
2 44047 98.0198 62.7893 0001012 76.3359 283.7961 14.72294083314091Epoch: 2024-12-26T07:10Z
Definitive object data (Epoch: 2024-12-26T07:10:04.39Z)
| Latitude | -0.00004° |
| Longitude | -140.00904° |
| Altitude | 656.592 km |
| Speed | 7.529 km/s |
| True Right ascension | 04h 11m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 78.53216° |
| Longitude | 83.90047° |
| Altitude | 666.303 km |
| Speed | 7.531 km/s |
| Apparent Right ascension | 22h 56m 01s |
| Apparent Declination | 27° 01' 10" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:51:52 |
| Azimuth | 13.389° NNE |
| Elevation | -21.813° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 651.522 km |
| Perigee altitude | 650.099 km |
| Semi-major axis | 7,028.948 km |
| Eccentricity | 0.0001012 |
| Inclination | 98.0198° |
| RAAN | 62.7893° |
| Arg. of periapsis | 76.3359° |
| True anomaly | 283.78484° |
| Mean anomaly | 283.7961° |
| Eccentric anomaly | 283.79047° |
| Mean motion | 3.68305 °/min |
| BSTAR | 0.00030373 |
| Orbital period | 97.75 mins |
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Other satellites on launch #8 in the year 2019 (2019-02-21 UTC)
| EGYPTSAT A, 44047 |
EGYPTSAT A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-26 17:32:21.300Z | 357.185° N | 2024-12-26 17:35:21.300Z | 261.368° W | 39.446° | 2024-12-26 17:38:21.300Z | 210.889° SW |
| 7 mins | 2024-12-27 04:30:21.300Z | 177.574° S | 2024-12-27 04:33:21.300Z | 279.847° WNW | 43.15° | 2024-12-27 04:37:21.300Z | 342.355° N |
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