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 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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 OBJECT F
1 63296U 25055F 26033.62025689 .00011717 00000-0 64889-3 0 9990
2 63296 97.6328 172.6066 0012035 228.0010 132.0197 15.13921544 48623Epoch: 2026-02-02T14:53Z
TLE epoch observation values (Epoch: 2026-02-02T14:53:10.195Z)
Latitude
-0.00002°
Longitude
176.50119°
Altitude
532.897 km
Speed
7.593 km/s
True Right ascension
11h 30m 25s
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
04:31:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.542 km
Perigee altitude
512.935 km
Semi-major axis
6,899.375 km
Eccentricity
0.0012
Inclination
97.6328°
RAAN
172.6066°
Arg. of periapsis
228.001°
True anomaly
132.12205°
Mean anomaly
132.0197°
Eccentric anomaly
132.07089°
Mean motion
3.78729 °/min
Orbital period
95.05 mins
BSTAR
0.00064889
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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 | 2026-02-03 08:28:53.754Z | 120.358° SE | 2026-02-03 08:30:53.754Z | 83.35° E | 23.116° | 2026-02-03 08:33:53.754Z | 19.863° NNE |
| 4 mins | 2026-02-03 10:03:53.754Z | 232.348° WSW | 2026-02-03 10:05:53.754Z | 273.014° WNW | 18.763° | 2026-02-03 10:07:53.754Z | 308.14° NW |
| 5 mins | 2026-02-03 21:36:53.754Z | 44.196° NE | 2026-02-03 21:38:53.754Z | 105.885° ESE | 32.122° | 2026-02-03 21:41:53.754Z | 166.594° S |
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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