OBJECT C, 65940
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT C, 65940 is a satellite owned by Shikong Daoyu (CN) in SSO that was launched on Sat, 11 Oct 2025 UTC via a YINLI-1 launch vehicle from the Yellow Sea Launch Area, China (YSLA). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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65940 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GWCG
Mission
Operational spacecraft
Bus & Motor
GSP50, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT C
1 65940U 25226C 25312.87134125 .00014556 00000-0 84971-3 0 9998
2 65940 97.6567 27.0533 0015236 178.8743 181.2524 15.11938445 4346Epoch: 2025-11-08T20:54Z
TLE epoch observation values (Epoch: 2025-11-08T20:54:43.884Z)
Latitude
-0.00006°
Longitude
25.07573°
Altitude
543.886 km
Speed
7.584 km/s
True Right ascension
01h 48m 12s
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
03:08:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.797 km
Perigee altitude
516.755 km
Semi-major axis
6,905.413 km
Eccentricity
0.00152
Inclination
97.6567°
RAAN
27.0533°
Arg. of periapsis
178.8743°
True anomaly
181.24859°
Mean anomaly
181.2524°
Eccentric anomaly
181.25049°
Mean motion
3.78232 °/min
Orbital period
95.18 mins
BSTAR
0.00084971
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Other satellites on launch #226 in the year 2025 (2025-10-11 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.OBJECT C 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 | 2025-11-10 17:56:46.376Z | 13.114° NNE | 2025-11-10 17:59:46.376Z | 23.064° NE | 43.7° | 2025-11-10 18:03:46.376Z | 192.178° SSW |
| 6 mins | 2025-11-11 04:38:46.376Z | 133.316° SE | 2025-11-11 04:41:46.376Z | 53.639° ENE | 30.684° | 2025-11-11 04:44:46.376Z | 4.73° 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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