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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Identifier
Orbit
Country
EG / 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: 1 day ago
TLE from 1 day ago
0 EGYPTSAT A
1 44047U 19008A 26180.51219115 .00000671 00000-0 11402-3 0 9994
2 44047 98.0196 245.1080 0001539 97.7380 262.4002 14.72321444395056Epoch: 2026-06-29T12:17Z
TLE epoch observation values (Epoch: 2026-06-29T12:17:33.315Z)
Latitude
-0.00003°
Longitude
143.12261°
Altitude
656.818 km
Speed
7.529 km/s
True Right ascension
16h 20m 25s
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
01:57:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.805 km
Perigee altitude
649.642 km
Semi-major axis
7,028.86 km
Eccentricity
0.00015
Inclination
98.0196°
RAAN
245.108°
Arg. of periapsis
97.738°
True anomaly
262.38272°
Mean anomaly
262.4002°
Eccentric anomaly
262.39146°
Mean motion
3.68312 °/min
Orbital period
97.74 mins
BSTAR
0.00011402
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-30 16:35:34.773Z | 32.662° NE | 2026-06-30 16:39:34.773Z | 99.526° ESE | 29.209° | 2026-06-30 16:42:34.773Z | 155.798° SSE |
| 4 mins | 2026-06-30 18:14:34.773Z | 320.113° NNW | 2026-06-30 18:15:34.773Z | 302.438° NW | 20.064° | 2026-06-30 18:18:34.773Z | 251.864° W |
| 6 mins | 2026-07-01 03:35:34.773Z | 115.183° SE | 2026-07-01 03:37:34.773Z | 77.889° E | 25.685° | 2026-07-01 03:41:34.773Z | 11.088° NNE |
| 5 mins | 2026-07-01 05:12:34.773Z | 225.835° WSW | 2026-07-01 05:14:34.773Z | 262.968° W | 22.806° | 2026-07-01 05:17:34.773Z | 313.508° NW |
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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