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). 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.
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44047 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EGYPRelated business
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
Shape & HBR
Box + 4 Pan + 1 Ant, 1.0 m
Radar Cross Section
0.867 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 EGYPTSAT A
1 44047U 19008A 25261.29836274 .00000606 00000-0 10358-3 0 9996
2 44047 98.0108 325.0744 0001280 109.2845 250.8501 14.72375230353233Epoch: 2025-09-18T07:09Z
TLE epoch observation values (Epoch: 2025-09-18T07:09:38.54Z)
Latitude
-0.00003°
Longitude
-139.79814°
Altitude
656.799 km
Speed
7.529 km/s
True Right ascension
21h 40m 17s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:43:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.451 km
Perigee altitude
649.652 km
Semi-major axis
7,028.689 km
Eccentricity
0.00013
Inclination
98.0108°
RAAN
325.0744°
Arg. of periapsis
109.2845°
True anomaly
250.83624°
Mean anomaly
250.8501°
Eccentric anomaly
250.84317°
Mean motion
3.68325 °/min
Orbital period
97.74 mins
BSTAR
0.00010358
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Other satellites on launch #8 in the year 2019 (2019-02-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EGYPTSAT A Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-19 04:29:54.416Z | 176.645° S | 2025-09-19 04:32:54.416Z | 286.082° WNW | 43.317° | 2025-09-19 04:36:54.416Z | 342.914° N |
| 5 mins | 2025-09-19 16:22:54.416Z | 54.27° ENE | 2025-09-19 16:24:54.416Z | 88.875° E | 21.983° | 2025-09-19 16:27:54.416Z | 140.802° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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