OBJECT B, 63292
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 B, 63292 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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63292 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: 17 hours ago
TLE from 17 hours ago
0 OBJECT B
1 63292U 25055B 25349.38984861 .00008965 00000-0 46593-3 0 9997
2 63292 97.6275 124.2347 0012717 77.2427 283.0226 15.16246730 41249Epoch: 2025-12-15T09:21Z
TLE epoch observation values (Epoch: 2025-12-15T09:21:22.919Z)
Latitude
-0.00004°
Longitude
-100.3999°
Altitude
518.309 km
Speed
7.605 km/s
True Right ascension
08h 16m 56s
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
00:58:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
522.942 km
Perigee altitude
505.412 km
Semi-major axis
6,892.314 km
Eccentricity
0.00127
Inclination
97.6275°
RAAN
124.2347°
Arg. of periapsis
77.2427°
True anomaly
282.88057°
Mean anomaly
283.0226°
Eccentric anomaly
282.95159°
Mean motion
3.79311 °/min
Orbital period
94.91 mins
BSTAR
0.00046593
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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 B 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 | 2025-12-16 09:14:09.704Z | 169.531° S | 2025-12-16 09:17:09.704Z | 195.606° SSW | 44.05° | 2025-12-16 09:20:09.704Z | 345.32° N |
| 6 mins | 2025-12-16 22:21:09.704Z | 356.089° N | 2025-12-16 22:23:09.704Z | 314.008° NW | 36.546° | 2025-12-16 22:27:09.704Z | 209.58° SW |
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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