DECAYED

CZ-3C R/B, 63925 (Decayed)

Orbit data source: Space-Track

CZ-3C R/B, 63925 was space debris in LEO originally from a launch on Mon, 12 May 2025 UTC launched from the Xichang Space Center, China (XSC). 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.

Not visible in the next 10 days
Identifier
63925, 2025-097B
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-05-12 (8 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 months ago

TLE from 4 months ago
0 CZ-3C R/B
1 63925U 25097B   25248.84348470  .58146912 -10351-4  15675-2 0  9994
2 63925  28.6678  63.8283 2235444 303.4300  37.1703 11.41187689  3056
Epoch: 2025-09-05T20:14Z
TLE epoch observation values (Epoch: 2025-09-05T20:14:37.078Z)
Latitude
0.00002°
Longitude
134.988°
Altitude
670.858 km
Speed
8.081 km/s
True Right ascension
04h 15m 18s
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
16:21:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,822.921 km
Perigee altitude
95.407 km
Semi-major axis
8,337.301 km
Eccentricity
0.22354
Inclination
28.6678°
RAAN
63.8283°
Arg. of periapsis
303.43°
True anomaly
56.62504°
Mean anomaly
37.1703°
Eccentric anomaly
46.45391°
Mean motion
2.85105 °/min
Orbital period
126.27 mins
BSTAR
0.0015675
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Other satellites on launch #97 in the year 2025 (2025-05-12 UTC)

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