CZ-6A R/B, 63922

Orbit data source: Space-Track

CZ-6A R/B, 63922 is space debris in LEO originally from a launch on Sun, 11 May 2025 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
63922, 2025-096E
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-6A STAGE 2, YF-115
Mass
~6,000 kg wet, ~6,000 kg dry
Launch date (UTC)
2025-05-11 (10 months ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 5.5 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 CZ-6A R/B
1 63922U 25096E   26061.77145967  .00000902  00000-0  16096-3 0  9991
2 63922  86.0159 225.0726 0070490 141.8698 218.7532 14.64071447 43131
Epoch: 2026-03-02T18:30Z
TLE epoch observation values (Epoch: 2026-03-02T18:30:54.115Z)
Latitude
-0.00007°
Longitude
146.78703°
Altitude
722.091 km
Speed
7.474 km/s
True Right ascension
15h 00m 17s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:14:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
726.72 km
Perigee altitude
627.257 km
Semi-major axis
7,055.126 km
Eccentricity
0.00705
Inclination
86.0159°
RAAN
225.0726°
Arg. of periapsis
141.8698°
True anomaly
218.25103°
Mean anomaly
218.7532°
Eccentric anomaly
218.50177°
Mean motion
3.66257 °/min
Orbital period
98.29 mins
BSTAR
0.00016096
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Other satellites on launch #96 in the year 2025 (2025-05-11 UTC)

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