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: 16 hours ago
TLE from 16 hours ago
0 EGYPTSAT A
1 44047U 19008A 25302.48330631 .00001007 00000-0 16713-3 0 9996
2 44047 98.0047 5.6385 0000930 92.8839 267.2475 14.72288976359292Epoch: 2025-10-29T11:35Z
TLE epoch observation values (Epoch: 2025-10-29T11:35:57.665Z)
Latitude
0.00001°
Longitude
153.59243°
Altitude
656.81 km
Speed
7.529 km/s
True Right ascension
00h 22m 33s
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
23:35:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.48 km
Perigee altitude
650.172 km
Semi-major axis
7,028.963 km
Eccentricity
0.00009
Inclination
98.0047°
RAAN
5.6385°
Arg. of periapsis
92.8839°
True anomaly
267.23686°
Mean anomaly
267.2475°
Eccentric anomaly
267.24218°
Mean motion
3.68304 °/min
Orbital period
97.75 mins
BSTAR
0.00016713
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Other satellites on launch #8 in the year 2019 (2019-02-21 UTC)
No other RSOs were in this launch
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-30 04:01:46.988Z | 150.731° SSE | 2025-10-30 04:05:46.988Z | 75.191° E | 40.011° | 2025-10-30 04:09:46.988Z | 357.05° N |
| 6 mins | 2025-10-30 17:32:46.988Z | 356.099° N | 2025-10-30 17:34:46.988Z | 312.969° NW | 39.255° | 2025-10-30 17:38:46.988Z | 210.345° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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