OBJECT C, 65940

Orbit data source: Space-Track

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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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Identifier
65940, 2025-226C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Flag of CNShikong Daoyi Keji YG (CN)
Manufacturer
GWCG
Mission
Operational Commercial Imaging
Bus & Motor
GSP50, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2025-10-11 (5 months ago)
Launch vehicle
YINLI-1
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Unknown
Shape & HBR
Box + 1 Pan, 1.1 m
Radar Cross Section
0.445 m²

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 OBJECT C
1 65940U 25226C   26069.53619951  .00011707  00000-0  64013-3 0  9996
2 65940  97.6395 149.1346 0015318 118.7577 241.5196 15.14339221 22741
Epoch: 2026-03-10T12:52Z
TLE epoch observation values (Epoch: 2026-03-10T12:52:07.637Z)
Latitude
0.00003°
Longitude
147.88939°
Altitude
531.116 km
Speed
7.594 km/s
True Right ascension
09h 56m 32s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:57:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.535 km
Perigee altitude
509.402 km
Semi-major axis
6,898.106 km
Eccentricity
0.00153
Inclination
97.6395°
RAAN
149.1346°
Arg. of periapsis
118.7577°
True anomaly
241.36545°
Mean anomaly
241.5196°
Eccentric anomaly
241.44251°
Mean motion
3.78834 °/min
Orbital period
95.03 mins
BSTAR
0.00064013
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Other satellites on launch #226 in the year 2025 (2025-10-11 UTC)

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