OBJECT A, 63208
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, 63208 is a satellite owned by Siwei (CN) in SSO that was launched on Sat, 15 Mar 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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63208 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
SAST
Mission
Operational Commercial Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
~1,000 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OBJECT A
1 63208U 25051A 25256.28868477 .00008976 00000-0 37469-3 0 9994
2 63208 97.4793 332.0637 0002182 86.6189 273.5298 15.23884277 27681Epoch: 2025-09-13T06:55Z
TLE epoch observation values (Epoch: 2025-09-13T06:55:42.364Z)
Latitude
0.00004°
Longitude
-124.38701°
Altitude
497.139 km
Speed
7.616 km/s
True Right ascension
22h 08m 15s
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
19:41:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.6 km
Perigee altitude
489.603 km
Semi-major axis
6,869.239 km
Eccentricity
0.00022
Inclination
97.4793°
RAAN
332.0637°
Arg. of periapsis
86.6189°
True anomaly
273.50484°
Mean anomaly
273.5298°
Eccentric anomaly
273.51732°
Mean motion
3.81224 °/min
Orbital period
94.43 mins
BSTAR
0.00037469
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Other satellites on launch #51 in the year 2025 (2025-03-15 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-14 05:06:29.683Z | 163.708° S | 2025-09-14 05:10:29.683Z | 8.941° NNE | 42.642° | 2025-09-14 05:13:29.683Z | 350.247° N |
| 5 mins | 2025-09-14 18:10:29.683Z | 1.571° NNE | 2025-09-14 18:12:29.683Z | 279.029° WNW | 42.901° | 2025-09-14 18:15:29.683Z | 202.195° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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