OBJECT F, 63296
Orbit data source: Space-Track
OBJECT F, 63296 is a Chinese satellite 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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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 0.7 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 OBJECT F
1 63296U 25055F 26166.54123490 .00007336 00000-0 37836-3 0 9991
2 63296 97.6528 306.3018 0012833 129.6180 230.6187 15.16586600 68751Epoch: 2026-06-15T12:59Z
TLE epoch observation values (Epoch: 2026-06-15T12:59:22.695Z)
Latitude
-0.00006°
Longitude
-152.3689°
Altitude
524.866 km
Speed
7.598 km/s
True Right ascension
20h 25m 12s
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
03:30:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.991 km
Perigee altitude
504.303 km
Semi-major axis
6,891.284 km
Eccentricity
0.00128
Inclination
97.6528°
RAAN
306.3018°
Arg. of periapsis
129.618°
True anomaly
230.50515°
Mean anomaly
230.6187°
Eccentric anomaly
230.56191°
Mean motion
3.79396 °/min
Orbital period
94.89 mins
BSTAR
0.00037836
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-15 21:28:37.968Z | 41.954° NE | 2026-06-15 21:31:37.968Z | 97.148° ESE | 21.366° | 2026-06-15 21:33:37.968Z | 139.043° SSE |
| 5 mins | 2026-06-16 09:42:37.968Z | 193.495° SSW | 2026-06-16 09:44:37.968Z | 243.818° WSW | 35.757° | 2026-06-16 09:47:37.968Z | 330.614° NNW |
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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