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: 18 hours ago
TLE from 18 hours ago
0 SHIYAN 24C 01
1 58650U 23206A 25291.71026514 .00003039 00000-0 26714-3 0 9990
2 58650 97.3776 267.3224 0001530 303.6899 56.4178 14.97233269 99160Epoch: 2025-10-18T17:02Z
TLE epoch observation values (Epoch: 2025-10-18T17:02:46.908Z)
Latitude
0.00002°
Longitude
-15.81043°
Altitude
577.921 km
Speed
7.572 km/s
True Right ascension
17h 49m 17s
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
06:07:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.508 km
Perigee altitude
571.381 km
Semi-major axis
6,950.582 km
Eccentricity
0.00015
Inclination
97.3776°
RAAN
267.3224°
Arg. of periapsis
303.6899°
True anomaly
56.43241°
Mean anomaly
56.4178°
Eccentric anomaly
56.4251°
Mean motion
3.74551 °/min
Orbital period
96.11 mins
BSTAR
0.00026714
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-19 11:15:20.037Z | 15.833° NNE | 2025-10-19 11:18:20.037Z | 45.689° ENE | 42.642° | 2025-10-19 11:22:20.037Z | 187.388° SSW |
| 5 mins | 2025-10-19 22:04:20.037Z | 125.033° SE | 2025-10-19 22:06:20.037Z | 66.647° ENE | 32.503° | 2025-10-19 22:09:20.037Z | 7.404° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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