OBJECT A, 63982
Orbit data source: Space-Track
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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OBJECT A
1 63982U 25100A 26192.14960179 .00004982 00000-0 22765-3 0 9991
2 63982 97.3668 264.3926 0026549 279.7068 80.1169 15.20713087 64285Epoch: 2026-07-11T03:35Z
TLE epoch observation values (Epoch: 2026-07-11T03:35:25.594Z)
Latitude
-0.00005°
Longitude
-78.531°
Altitude
503.691 km
Speed
7.614 km/s
True Right ascension
17h 37m 34s
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
02:36:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.914 km
Perigee altitude
482.389 km
Semi-major axis
6,878.789 km
Eccentricity
0.00265
Inclination
97.3668°
RAAN
264.3926°
Arg. of periapsis
279.7068°
True anomaly
80.41678°
Mean anomaly
80.1169°
Eccentric anomaly
80.26682°
Mean motion
3.8043 °/min
Orbital period
94.63 mins
BSTAR
0.00022765
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-11 16:49:00.810Z | 61.983° ENE | 2026-07-11 16:51:00.810Z | 99.834° ESE | 16.476° | 2026-07-11 16:53:00.810Z | 133.703° SE |
| 4 mins | 2026-07-11 18:23:00.810Z | 328.221° NNW | 2026-07-11 18:25:00.810Z | 274.66° WNW | 24.923° | 2026-07-11 18:27:00.810Z | 235.628° WSW |
| 5 mins | 2026-07-12 05:00:00.810Z | 175.149° S | 2026-07-12 05:02:00.810Z | 259.594° W | 44.3° | 2026-07-12 05:05:00.810Z | 344.168° N |
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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