OBJECT A, 65945
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, 65945 is a satellite owned by CAST (CN) in LEO that was launched on Mon, 13 Oct 2025 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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65945 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational spacecraft
Bus & Motor
SY30, Unknown motor
Mass
~1,000 kg wet, ~1,000 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: 14 hours ago
TLE from 14 hours ago
0 OBJECT A
1 65945U 25227A 25340.61640756 .00013781 00000-0 61406-3 0 9996
2 65945 80.0051 30.1913 0011744 94.7221 265.5348 15.21280581 8244Epoch: 2025-12-06T14:47Z
TLE epoch observation values (Epoch: 2025-12-06T14:47:37.613Z)
Latitude
0.00002°
Longitude
92.643°
Altitude
505.621 km
Speed
7.611 km/s
True Right ascension
02h 00m 45s
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
02:34:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.147 km
Perigee altitude
490.994 km
Semi-major axis
6,877.208 km
Eccentricity
0.00117
Inclination
80.0051°
RAAN
30.1913°
Arg. of periapsis
94.7221°
True anomaly
265.40065°
Mean anomaly
265.5348°
Eccentric anomaly
265.46772°
Mean motion
3.80562 °/min
Orbital period
94.6 mins
BSTAR
0.00061406
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Other satellites on launch #227 in the year 2025 (2025-10-13 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 | 2025-12-07 05:08:58.108Z | 240.661° WSW | 2025-12-07 05:10:58.108Z | 280.472° WNW | 21.79° | 2025-12-07 05:13:58.108Z | 339.938° N |
| 5 mins | 2025-12-07 15:02:58.108Z | 4.036° NNE | 2025-12-07 15:04:58.108Z | 98.176° ESE | 41.608° | 2025-12-07 15:07:58.108Z | 159.233° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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