SHIYAN 24C 02, 58651
Orbit data source: Space-Track
SHIYAN 24C 02, 58651 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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58651 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: 15 hours ago
TLE from 15 hours ago
0 SHIYAN 24C 02
1 58651U 23206B 26031.74872723 .00003369 00000-0 29182-3 0 9996
2 58651 97.3915 6.6291 0001914 128.2914 231.8481 14.97741515114880Epoch: 2026-01-31T17:58Z
TLE epoch observation values (Epoch: 2026-01-31T17:58:10.032Z)
Latitude
-0.00008°
Longitude
-33.88095°
Altitude
577.759 km
Speed
7.571 km/s
True Right ascension
00h 26m 30s
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
11:06:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.201 km
Perigee altitude
569.541 km
Semi-major axis
6,949.008 km
Eccentricity
0.00019
Inclination
97.3915°
RAAN
6.6291°
Arg. of periapsis
128.2914°
True anomaly
231.83086°
Mean anomaly
231.8481°
Eccentric anomaly
231.83948°
Mean motion
3.74679 °/min
Orbital period
96.08 mins
BSTAR
0.00029182
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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 02 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 | 2026-02-01 10:34:08.323Z | 29.43° NE | 2026-02-01 10:38:08.323Z | 111.194° ESE | 31.023° | 2026-02-01 10:41:08.323Z | 164.302° S |
| 5 mins | 2026-02-01 21:23:08.323Z | 107.06° ESE | 2026-02-01 21:25:08.323Z | 69.673° E | 20.262° | 2026-02-01 21:28:08.323Z | 19.98° NNE |
| 5 mins | 2026-02-01 22:58:08.323Z | 218.926° SW | 2026-02-01 23:00:08.323Z | 261.14° W | 24.744° | 2026-02-01 23:03:08.323Z | 318.47° 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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