SHIKONGXING 01, 65712
Orbit data source: Space-Track
SHIKONGXING 01, 65712 is a Chinese payload satellite in LEO that was launched on Wed, 24 Sep 2025 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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65712 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Shikong Daoyu
Mission
Operational Commercial Navigation
Bus & Motor
GPS50, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SHIKONGXING 01
1 65712U 25214A 26171.34057756 .00001804 00000-0 19567-3 0 9993
2 65712 49.9872 279.1883 0013562 261.3506 98.5900 14.92852450 40173Epoch: 2026-06-20T08:10Z
TLE epoch observation values (Epoch: 2026-06-20T08:10:25.901Z)
Latitude
0.00002°
Longitude
-111.97621°
Altitude
591.015 km
Speed
7.565 km/s
True Right ascension
18h 36m 45s
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
07:13:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
599.26 km
Perigee altitude
580.36 km
Semi-major axis
6,967.947 km
Eccentricity
0.00136
Inclination
49.9872°
RAAN
279.1883°
Arg. of periapsis
261.3506°
True anomaly
98.74363°
Mean anomaly
98.59°
Eccentric anomaly
98.66682°
Mean motion
3.73152 °/min
Orbital period
96.48 mins
BSTAR
0.00019567
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Other satellites on launch #214 in the year 2025 (2025-09-24 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.SHIKONGXING 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 | 2026-06-21 10:04:16.408Z | 228.63° WSW | 2026-06-21 10:07:16.408Z | 185.27° SSW | 44.082° | 2026-06-21 10:11:16.408Z | 58.281° ENE |
| 6 mins | 2026-06-21 11:46:16.408Z | 294.284° NW | 2026-06-21 11:48:16.408Z | 333.384° NNW | 26.316° | 2026-06-21 11:52:16.408Z | 42.956° NE |
| 5 mins | 2026-06-21 13:28:16.408Z | 326.175° NNW | 2026-06-21 13:30:16.408Z | 1.322° NNE | 20.469° | 2026-06-21 13:33:16.408Z | 49.778° ENE |
| 6 mins | 2026-06-21 15:09:16.408Z | 323.351° NNW | 2026-06-21 15:12:16.408Z | 33.667° NE | 31.957° | 2026-06-21 15:15:16.408Z | 88.438° E |
| 6 mins | 2026-06-21 16:50:16.408Z | 285.144° WNW | 2026-06-21 16:53:16.408Z | 200.579° SSW | 35.312° | 2026-06-21 16:56:16.408Z | 150.766° 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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