OBJECT-A, 65488
Orbit data source: Space-Track
OBJECT-A, 65488 is a Chinese satellite in SSO that was launched on Fri, 05 Sep 2025 UTC via a GUSHENXING 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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65488 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT-A
1 65488U 25197A 26155.01114350 .00002992 00000-0 18584-3 0 9990
2 65488 97.4127 337.5891 0015264 76.0526 284.2400 15.10328749 41020Epoch: 2026-06-04T00:16Z
TLE epoch observation values (Epoch: 2026-06-04T00:16:02.798Z)
Latitude
-0.00005°
Longitude
81.11591°
Altitude
535.692 km
Speed
7.596 km/s
True Right ascension
22h 30m 21s
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
10:52:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.724 km
Perigee altitude
521.628 km
Semi-major axis
6,910.313 km
Eccentricity
0.00153
Inclination
97.4127°
RAAN
337.5891°
Arg. of periapsis
76.0526°
True anomaly
284.07038°
Mean anomaly
284.24°
Eccentric anomaly
284.1552°
Mean motion
3.7783 °/min
Orbital period
95.28 mins
BSTAR
0.00018584
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Other satellites on launch #197 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 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-06 12:50:06.938Z | 221.306° SW | 2026-06-06 12:52:06.938Z | 276.304° WNW | 26.162° | 2026-06-06 12:54:06.938Z | 317.215° NNW |
| 4 mins | 2026-06-07 00:25:06.938Z | 62.56° ENE | 2026-06-07 00:26:06.938Z | 87.53° E | 24.73° | 2026-06-07 00:29:06.938Z | 150.904° SSE |
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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