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: 9 hours ago
TLE from 9 hours ago
0 OBJECT F
1 63296U 25055F 25258.65406424 .00013846 00000-0 85114-3 0 9990
2 63296 97.6233 32.7843 0013073 353.8810 6.2258 15.10100640 27478Epoch: 2025-09-15T15:41Z
TLE epoch observation values (Epoch: 2025-09-15T15:41:51.15Z)
Latitude
0.00005°
Longitude
162.46555°
Altitude
529.976 km
Speed
7.603 km/s
True Right ascension
02h 11m 08s
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
17:00:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.916 km
Perigee altitude
523.846 km
Semi-major axis
6,911.018 km
Eccentricity
0.00131
Inclination
97.6233°
RAAN
32.7843°
Arg. of periapsis
353.881°
True anomaly
6.24207°
Mean anomaly
6.2258°
Eccentric anomaly
6.23393°
Mean motion
3.77772 °/min
Orbital period
95.3 mins
BSTAR
0.00085114
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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 | 2025-09-16 09:19:20.070Z | 185.56° SSW | 2025-09-16 09:22:20.070Z | 288.08° WNW | 38.413° | 2025-09-16 09:25:20.070Z | 337.797° N |
| 5 mins | 2025-09-16 22:29:20.070Z | 338.082° N | 2025-09-16 22:31:20.070Z | 286.497° WNW | 29.031° | 2025-09-16 22:34:20.070Z | 226.511° WSW |
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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