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.

Loading next visibility...
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 (8 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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago
0 OBJECT C
1 65940U 25226C   26155.13124748  .00008898  00000-0  46942-3 0  9991
2 65940  97.6347 235.1175 0013693 178.2005 181.9279 15.15711661 35707
Epoch: 2026-06-04T03:08Z
TLE epoch observation values (Epoch: 2026-06-04T03:08:59.782Z)
Latitude
Longitude
-64.71151°
Altitude
531.338 km
Speed
7.592 km/s
True Right ascension
15h 40m 28s
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
12:26:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
525.24 km
Perigee altitude
506.36 km
Semi-major axis
6,893.937 km
Eccentricity
0.00137
Inclination
97.6347°
RAAN
235.1175°
Arg. of periapsis
178.2005°
True anomaly
181.92263°
Mean anomaly
181.9279°
Eccentric anomaly
181.92526°
Mean motion
3.79177 °/min
Orbital period
94.94 mins
BSTAR
0.00046942
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #226 in the year 2025 (2025-10-11 UTC)

Documentation

Showing up to 5 results
|