OBJECT A, 65486
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, 65486 is a satellite owned by CNSA (CN) in GEO that was launched on Fri, 05 Sep 2025 UTC via a CHANG ZHENG 3C/YZ-1 launch vehicle from the Xichang Space Center, China (XSC). 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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65486 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
IMI/CAS
Mission
Operational spacecraft
Bus & Motor
SECM3000, AKM?
Mass
~1,150 kg wet, ~850 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OBJECT A
1 65486U 25196A 25259.58447578 -.00000252 00000-0 00000-0 0 9993
2 65486 28.5221 21.9757 0089948 131.1917 219.4438 0.98868954 135Epoch: 2025-09-16T14:01Z
TLE epoch observation values (Epoch: 2025-09-16T14:01:38.707Z)
Latitude
-4.76694°
Longitude
166.95403°
Altitude
36,483.875 km
Speed
3.039 km/s
True Right ascension
00h 52m 33s
True Declination
-4° 45' 44"
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
02:55:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,568.058 km
Perigee altitude
35,802.36 km
Semi-major axis
42,563.346 km
Eccentricity
0.00899
Inclination
28.5221°
RAAN
21.9757°
Arg. of periapsis
131.1917°
True anomaly
218.79461°
Mean anomaly
219.4438°
Eccentric anomaly
219.11864°
Mean motion
0.24717 °/min
Orbital period
1,456.51 mins
BSTAR
0
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Other satellites on launch #196 in the year 2025 (2025-09-05 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
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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. |
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| OBJECT A is likely not visible in the next few days. |
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65486 neighbors
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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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