HORUS 2, 55844
Orbit data source: Space-Track
HORUS 2, 55844 is a payload satellite owned by EgSA (EG) in SSO that was launched on Mon, 13 Mar 2023 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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55844 intel report (Beta)
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Identifier
Orbit
Country
EG / EGYPRelated business
Manufacturer
DFH
Mission
Operational Defense Imaging
Bus & Motor
CAST-2000?, Unknown motor
Mass
~330 kg wet, ~330 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
2.815 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 HORUS 2
1 55844U 23032A 26172.52358841 .00004101 00000-0 17498-3 0 9998
2 55844 97.3531 247.8379 0002298 101.9753 258.1742 15.23463726182147Epoch: 2026-06-21T12:33Z
TLE epoch observation values (Epoch: 2026-06-21T12:33:58.038Z)
Latitude
-0.00002°
Longitude
149.62344°
Altitude
498.823 km
Speed
7.615 km/s
True Right ascension
16h 31m 21s
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
21:34:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.94 km
Perigee altitude
490.783 km
Semi-major axis
6,870.498 km
Eccentricity
0.00023
Inclination
97.3531°
RAAN
247.8379°
Arg. of periapsis
101.9753°
True anomaly
258.14843°
Mean anomaly
258.1742°
Eccentric anomaly
258.16131°
Mean motion
3.81119 °/min
Orbital period
94.46 mins
BSTAR
0.00017498
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Other satellites on launch #32 in the year 2023 (2023-03-13 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.HORUS 2 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 17:30:53.444Z | 34.388° NE | 2026-06-22 17:32:53.444Z | 78.939° E | 31.978° | 2026-06-22 17:35:53.444Z | 164.065° S |
| 4 mins | 2026-06-23 05:41:53.444Z | 222.932° SW | 2026-06-23 05:42:53.444Z | 248.291° W | 25.309° | 2026-06-23 05:45:53.444Z | 319.243° NNW |
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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