OBJECT B, 65939
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 B, 65939 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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65939 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GWCG
Mission
Operational spacecraft
Bus & Motor
GSP50, Unknown motor
Mass
~50 kg wet, ~50 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: 3 days ago
TLE from 3 days ago
0 OBJECT B
1 65939U 25226B 25288.11449019 .00006878 00000-0 41438-3 0 9995
2 65939 97.6635 2.2519 0013950 262.6480 97.3164 15.11034630 605Epoch: 2025-10-15T02:44Z
TLE epoch observation values (Epoch: 2025-10-15T02:44:51.952Z)
Latitude
-0.00004°
Longitude
-62.85777°
Altitude
537.355 km
Speed
7.593 km/s
True Right ascension
00h 09m 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
21:28:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.669 km
Perigee altitude
520.395 km
Semi-major axis
6,908.169 km
Eccentricity
0.0014
Inclination
97.6635°
RAAN
2.2519°
Arg. of periapsis
262.648°
True anomaly
97.47492°
Mean anomaly
97.3164°
Eccentric anomaly
97.39566°
Mean motion
3.78006 °/min
Orbital period
95.24 mins
BSTAR
0.00041438
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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 B 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 05:35:16.961Z | 209.994° SW | 2025-10-18 05:37:16.961Z | 269.725° W | 31.291° | 2025-10-18 05:40:16.961Z | 328.303° NNW |
| 4 mins | 2025-10-18 17:10:16.961Z | 66.556° ENE | 2025-10-18 17:11:16.961Z | 87.847° E | 20.362° | 2025-10-18 17:14:16.961Z | 143.908° SSE |
| 4 mins | 2025-10-18 18:44:16.961Z | 326.093° NNW | 2025-10-18 18:46:16.961Z | 280.536° WNW | 21.874° | 2025-10-18 18:48:16.961Z | 243.453° WSW |
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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