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: 9 hours ago
TLE from 9 hours ago
0 OBJECT A
1 65938U 25226A 25340.92106992 .00013233 00000-0 75448-3 0 9993
2 65938 97.6634 55.2517 0016118 90.5950 269.7128 15.12800456 8597Epoch: 2025-12-06T22:06Z
TLE epoch observation values (Epoch: 2025-12-06T22:06:20.441Z)
Latitude
0.00006°
Longitude
7.72464°
Altitude
530.811 km
Speed
7.597 km/s
True Right ascension
03h 41m 00s
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
05:39:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.777 km
Perigee altitude
513.525 km
Semi-major axis
6,902.788 km
Eccentricity
0.00161
Inclination
97.6634°
RAAN
55.2517°
Arg. of periapsis
90.595°
True anomaly
269.52811°
Mean anomaly
269.7128°
Eccentric anomaly
269.62045°
Mean motion
3.78448 °/min
Orbital period
95.13 mins
BSTAR
0.00075448
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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 | 2025-12-07 17:42:48.318Z | 23.024° NE | 2025-12-07 17:46:48.318Z | 130.277° SE | 36.649° | 2025-12-07 17:49:48.318Z | 177.078° S |
| 4 mins | 2025-12-08 04:25:48.318Z | 104.437° ESE | 2025-12-08 04:26:48.318Z | 82.702° E | 21.674° | 2025-12-08 04:29:48.318Z | 20.784° NNE |
| 4 mins | 2025-12-08 05:59:48.318Z | 229.961° WSW | 2025-12-08 06:01:48.318Z | 271.775° WNW | 19.302° | 2025-12-08 06:03:48.318Z | 308.389° NW |
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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