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 (7 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: 10 hours ago

TLE from 10 hours ago
0 CZ-6A R/B
1 63922U 25096E   25334.56734744  .00000621  00000-0  10955-3 0  9993
2 63922  86.0162 269.7713 0071657  97.0581 263.8787 14.63931702 29646
Epoch: 2025-11-30T13:36Z
TLE epoch observation values (Epoch: 2025-11-30T13:36:58.818Z)
Latitude
-0.00002°
Longitude
-4.15312°
Altitude
689.348 km
Speed
7.509 km/s
True Right ascension
17h 59m 05s
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
21:17:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
727.996 km
Perigee altitude
626.88 km
Semi-major axis
7,055.575 km
Eccentricity
0.00717
Inclination
86.0162°
RAAN
269.7713°
Arg. of periapsis
97.0581°
True anomaly
263.06306°
Mean anomaly
263.8787°
Eccentric anomaly
263.4708°
Mean motion
3.66222 °/min
Orbital period
98.3 mins
BSTAR
0.00010955
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Other satellites on launch #96 in the year 2025 (2025-05-11 UTC)

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