OBJECT A, 65938
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 A, 65938 is a satellite owned by Changguang WJ (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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65938 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational spacecraft
Bus & Motor
JL-1, Unknown motor
Mass
230 kg wet, ~200 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 A
1 65938U 25226A 25312.86921177 .00014555 00000-0 84700-3 0 9994
2 65938 97.6658 27.0882 0015275 180.8284 179.2923 15.12051604 4352Epoch: 2025-11-08T20:51Z
TLE epoch observation values (Epoch: 2025-11-08T20:51:39.896Z)
Latitude
-0.00009°
Longitude
25.87934°
Altitude
543.57 km
Speed
7.585 km/s
True Right ascension
01h 48m 21s
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
03:53:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.479 km
Perigee altitude
516.384 km
Semi-major axis
6,905.069 km
Eccentricity
0.00153
Inclination
97.6658°
RAAN
27.0882°
Arg. of periapsis
180.8284°
True anomaly
179.29446°
Mean anomaly
179.2923°
Eccentric anomaly
179.29338°
Mean motion
3.78261 °/min
Orbital period
95.17 mins
BSTAR
0.000847
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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 A 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 17:53:20.933Z | 15.176° NNE | 2025-11-10 17:57:20.933Z | 165.465° S | 42.249° | 2025-11-10 18:00:20.933Z | 188.82° SSW |
| 5 mins | 2025-11-11 04:36:20.933Z | 118.882° SE | 2025-11-11 04:38:20.933Z | 60.431° ENE | 29.253° | 2025-11-11 04:41:20.933Z | 7.425° NNE |
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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