OBJECT L, 63992
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 L, 63992 is a Chinese satellite in SSO that was launched on Wed, 14 May 2025 UTC via a CHANG ZHENG 2D 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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63992 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.9 m
Radar Cross Section
0.135 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 OBJECT L
1 63992U 25100L 25340.82274550 .00031979 00000-0 14616-2 0 9993
2 63992 97.3898 52.9072 0011904 244.6681 115.3322 15.20430105 31389Epoch: 2025-12-06T19:44Z
TLE epoch observation values (Epoch: 2025-12-06T19:44:45.211Z)
Latitude
0°
Longitude
40.87386°
Altitude
511.148 km
Speed
7.606 km/s
True Right ascension
03h 31m 37s
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
14:27:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.696 km
Perigee altitude
493.317 km
Semi-major axis
6,879.644 km
Eccentricity
0.00119
Inclination
97.3898°
RAAN
52.9072°
Arg. of periapsis
244.6681°
True anomaly
115.45541°
Mean anomaly
115.3322°
Eccentric anomaly
115.39382°
Mean motion
3.80359 °/min
Orbital period
94.65 mins
BSTAR
0.0014616
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Other satellites on launch #100 in the year 2025 (2025-05-14 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 L 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-07 18:26:29.454Z | 327.411° NNW | 2025-12-07 18:27:29.454Z | 300.664° NW | 26.784° | 2025-12-07 18:30:29.454Z | 230.545° WSW |
| 5 mins | 2025-12-08 05:03:29.454Z | 169.805° S | 2025-12-08 05:05:29.454Z | 277.113° WNW | 44.916° | 2025-12-08 05:08:29.454Z | 346.798° N |
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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