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 (1 year 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: 14 hours ago

TLE from 14 hours ago
0 CZ-6A R/B
1 63922U 25096E   26171.39558341  .00000317  00000-0  53322-4 0  9999
2 63922  86.0186 171.9901 0070858 128.5328 232.2264 14.64167157 59173
Epoch: 2026-06-20T09:29Z
TLE epoch observation values (Epoch: 2026-06-20T09:29:38.406Z)
Latitude
-0.00012°
Longitude
120.96925°
Altitude
713.699 km
Speed
7.482 km/s
True Right ascension
11h 27m 57s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
10:20:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
726.67 km
Perigee altitude
626.692 km
Semi-major axis
7,054.818 km
Eccentricity
0.00709
Inclination
86.0186°
RAAN
171.9901°
Arg. of periapsis
128.5328°
True anomaly
231.58806°
Mean anomaly
232.2264°
Eccentric anomaly
231.90688°
Mean motion
3.66281 °/min
Orbital period
98.29 mins
BSTAR
0.000053322
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Other satellites on launch #96 in the year 2025 (2025-05-11 UTC)

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