OBJECT A, 65259
Orbit data source: Space-Track
OBJECT A, 65259 is a Chinese satellite in SSO that was launched on Tue, 19 Aug 2025 UTC via a LIJIAN-1 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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65259 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Radar Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 1.1 m
Radar Cross Section
3.533 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT A
1 65259U 25180A 26169.58202126 .00012758 00000-0 54378-3 0 9996
2 65259 97.5211 298.4346 0010810 311.7658 48.2654 15.23032458 46003Epoch: 2026-06-18T13:58Z
TLE epoch observation values (Epoch: 2026-06-18T13:58:06.636Z)
Latitude
-0.00002°
Longitude
-177.91633°
Altitude
494.847 km
Speed
7.62 km/s
True Right ascension
19h 53m 44s
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
07:19:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.095 km
Perigee altitude
486.238 km
Semi-major axis
6,871.804 km
Eccentricity
0.00108
Inclination
97.5211°
RAAN
298.4346°
Arg. of periapsis
311.7658°
True anomaly
48.35792°
Mean anomaly
48.2654°
Eccentric anomaly
48.31165°
Mean motion
3.81011 °/min
Orbital period
94.49 mins
BSTAR
0.00054378
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Other satellites on launch #180 in the year 2025 (2025-08-19 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 21:42:48.209Z | 2.309° NNE | 2026-06-20 21:45:48.209Z | 292.351° WNW | 40.358° | 2026-06-20 21:48:48.209Z | 207.906° SW |
| 5 mins | 2026-06-21 08:20:48.209Z | 133.105° SE | 2026-06-21 08:22:48.209Z | 50.241° ENE | 35.337° | 2026-06-21 08:25:48.209Z | 0.075° NNE |
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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