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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OBJECT A
1 65938U 25226A 25290.43097179 .00013308 00000-0 78752-3 0 9993
2 65938 97.6683 4.5777 0014141 261.4311 98.5317 15.11483179 969Epoch: 2025-10-17T10:20Z
TLE epoch observation values (Epoch: 2025-10-17T10:20:35.962Z)
Latitude
0.00001°
Longitude
-176.74859°
Altitude
536.211 km
Speed
7.594 km/s
True Right ascension
00h 18m 18s
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
21:28:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.431 km
Perigee altitude
518.898 km
Semi-major axis
6,906.802 km
Eccentricity
0.00141
Inclination
97.6683°
RAAN
4.5777°
Arg. of periapsis
261.4311°
True anomaly
98.69191°
Mean anomaly
98.5317°
Eccentric anomaly
98.61181°
Mean motion
3.78118 °/min
Orbital period
95.21 mins
BSTAR
0.00078752
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-18 05:33:17.374Z | 209.341° SW | 2025-10-18 05:35:17.374Z | 274.703° WNW | 32.287° | 2025-10-18 05:38:17.374Z | 330.295° NNW |
| 4 mins | 2025-10-18 18:42:17.374Z | 321.434° NNW | 2025-10-18 18:43:17.374Z | 298.071° NW | 23.119° | 2025-10-18 18:46:17.374Z | 238.167° WSW |
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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