OBJECT F, 63296
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 F, 63296 is a satellite owned by Yunyao yuhang (CN) in SSO that was launched on Mon, 17 Mar 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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63296 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Changguang WJ
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
YY-1, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT F
1 63296U 25055F 25256.33484438 .00006503 00000-0 40275-3 0 9995
2 63296 97.6234 30.4771 0013154 2.0849 358.0433 15.10058372 27128Epoch: 2025-09-13T08:02Z
TLE epoch observation values (Epoch: 2025-09-13T08:02:10.554Z)
Latitude
0.00002°
Longitude
-82.63656°
Altitude
530.001 km
Speed
7.603 km/s
True Right ascension
02h 01m 54s
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
10:36:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.101 km
Perigee altitude
523.919 km
Semi-major axis
6,911.147 km
Eccentricity
0.00132
Inclination
97.6234°
RAAN
30.4771°
Arg. of periapsis
2.0849°
True anomaly
358.03814°
Mean anomaly
358.0433°
Eccentric anomaly
358.04072°
Mean motion
3.77762 °/min
Orbital period
95.3 mins
BSTAR
0.00040275
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Other satellites on launch #55 in the year 2025 (2025-03-17 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 F 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 | 2025-09-13 21:19:38.273Z | 35.383° NE | 2025-09-13 21:22:38.273Z | 91.73° ESE | 27.679° | 2025-09-13 21:25:38.273Z | 156.216° SSE |
| 5 mins | 2025-09-14 09:37:38.273Z | 217.672° SW | 2025-09-14 09:39:38.273Z | 276.208° WNW | 28.078° | 2025-09-14 09:42:38.273Z | 327.616° NNW |
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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