OBJECT A, 63982
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 A, 63982 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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63982 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, 0.8 m
Radar Cross Section
0.195 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 A
1 63982U 25100A 25312.85961575 .00019677 00000-0 85732-3 0 9993
2 63982 97.3922 25.1759 0009627 63.6805 296.5419 15.22194665 27155Epoch: 2025-11-08T20:37Z
TLE epoch observation values (Epoch: 2025-11-08T20:37:50.800Z)
Latitude
-0.00005°
Longitude
27.43106°
Altitude
499.362 km
Speed
7.616 km/s
True Right ascension
01h 40m 42s
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
20:39:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.802 km
Perigee altitude
489.567 km
Semi-major axis
6,874.322 km
Eccentricity
0.00096
Inclination
97.3922°
RAAN
25.1759°
Arg. of periapsis
63.6805°
True anomaly
296.44316°
Mean anomaly
296.5419°
Eccentric anomaly
296.49253°
Mean motion
3.80801 °/min
Orbital period
94.54 mins
BSTAR
0.00085732
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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 A 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 | 2025-11-09 04:39:06.558Z | 144.025° SSE | 2025-11-09 04:42:06.558Z | 66.168° ENE | 35.096° | 2025-11-09 04:45:06.558Z | 2.629° NNE |
| 5 mins | 2025-11-09 17:43:06.558Z | 21.489° NNE | 2025-11-09 17:45:06.558Z | 95.787° ESE | 43.284° | 2025-11-09 17:48:06.558Z | 184.413° SSW |
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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