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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 12 hours ago
TLE from 12 hours ago
0 HORUS 2
1 55844U 23032A 25306.51091742 .00008381 00000-0 35305-3 0 9990
2 55844 97.3791 21.1520 0004501 135.4796 224.6803 15.23583686146979Epoch: 2025-11-02T12:15Z
TLE epoch observation values (Epoch: 2025-11-02T12:15:43.265Z)
Latitude
-0.00004°
Longitude
155.19613°
Altitude
500.338 km
Speed
7.613 km/s
True Right ascension
01h 24m 36s
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
20:28:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.094 km
Perigee altitude
488.909 km
Semi-major axis
6,870.139 km
Eccentricity
0.00045
Inclination
97.3791°
RAAN
21.152°
Arg. of periapsis
135.4796°
True anomaly
224.64405°
Mean anomaly
224.6803°
Eccentric anomaly
224.66217°
Mean motion
3.81149 °/min
Orbital period
94.45 mins
BSTAR
0.00035305
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-03 04:10:44.862Z | 105.205° ESE | 2025-11-03 04:12:44.862Z | 71.183° E | 15.151° | 2025-11-03 04:14:44.862Z | 34.986° NE |
| 4 mins | 2025-11-03 05:44:44.862Z | 219.979° SW | 2025-11-03 05:46:44.862Z | 277.515° WNW | 25.981° | 2025-11-03 05:48:44.862Z | 318.733° NNW |
| 4 mins | 2025-11-03 17:13:44.862Z | 65.257° ENE | 2025-11-03 17:14:44.862Z | 87.251° E | 19.558° | 2025-11-03 17:17:44.862Z | 144.922° SSE |
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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