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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT A
1 65945U 25227A 25290.80515056 .00009515 00000-0 43926-3 0 9992
2 65945 80.0018 96.1165 0011192 253.9339 106.0655 15.20070888 679Epoch: 2025-10-17T19:19Z
TLE epoch observation values (Epoch: 2025-10-17T19:19:25.008Z)
Latitude
-0.00007°
Longitude
139.71704°
Altitude
510.771 km
Speed
7.607 km/s
True Right ascension
06h 24m 27s
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
21:30:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.423 km
Perigee altitude
495.021 km
Semi-major axis
6,880.859 km
Eccentricity
0.00112
Inclination
80.0018°
RAAN
96.1165°
Arg. of periapsis
253.9339°
True anomaly
106.18869°
Mean anomaly
106.0655°
Eccentric anomaly
106.1271°
Mean motion
3.80259 °/min
Orbital period
94.67 mins
BSTAR
0.00043926
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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 | 2025-10-18 11:15:30.337Z | 134.526° SE | 2025-10-18 11:17:30.337Z | 97.303° ESE | 19.611° | 2025-10-18 11:20:30.337Z | 43.641° NE |
| 4 mins | 2025-10-18 12:51:30.337Z | 249.08° W | 2025-10-18 12:53:30.337Z | 291.587° WNW | 20.939° | 2025-10-18 12:55:30.337Z | 331.223° NNW |
| 5 mins | 2025-10-18 22:45:30.337Z | 358.191° N | 2025-10-18 22:47:30.337Z | 85.29° E | 43.717° | 2025-10-18 22:50:30.337Z | 162.796° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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