SHIYAN 24C 01, 58650
Orbit data source: Space-Track
SHIYAN 24C 01, 58650 is a payload satellite owned by CASC (CN) in SSO that was launched on Mon, 25 Dec 2023 UTC via a CHANG ZHENG 11 launch vehicle from the South China Sea Launch Area (SCSLA). 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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58650 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM?
Mission
Operational Defense Technology
Bus & Motor
Unknown
Mass
~80 kg wet, ~80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 4.0 m
Radar Cross Section
8.634 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SHIYAN 24C 01
1 58650U 23206A 25306.68011536 .00003086 00000-0 27059-3 0 9996
2 58650 97.3791 281.4583 0002093 186.6950 173.4246 14.97326243101406Epoch: 2025-11-02T16:19Z
TLE epoch observation values (Epoch: 2025-11-02T16:19:21.967Z)
Latitude
0.00007°
Longitude
-5.57561°
Altitude
579.668 km
Speed
7.57 km/s
True Right ascension
18h 45m 49s
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
02:03:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.611 km
Perigee altitude
570.702 km
Semi-major axis
6,950.294 km
Eccentricity
0.00021
Inclination
97.3791°
RAAN
281.4583°
Arg. of periapsis
186.695°
True anomaly
173.42735°
Mean anomaly
173.4246°
Eccentric anomaly
173.42597°
Mean motion
3.74575 °/min
Orbital period
96.11 mins
BSTAR
0.00027059
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Other satellites on launch #206 in the year 2023 (2023-12-25 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.SHIYAN 24C 01 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 | 2025-11-03 10:32:57.930Z | 46.391° ENE | 2025-11-03 10:35:57.930Z | 104.18° ESE | 22.287° | 2025-11-03 10:37:57.930Z | 140.906° SSE |
| 5 mins | 2025-11-03 12:08:57.930Z | 327.257° NNW | 2025-11-03 12:10:57.930Z | 285.294° WNW | 22.103° | 2025-11-03 12:13:57.930Z | 236.879° WSW |
| 6 mins | 2025-11-03 22:55:57.930Z | 200.441° SSW | 2025-11-03 22:57:57.930Z | 248.24° W | 33.803° | 2025-11-03 23:01:57.930Z | 333.133° 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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