CZ-3B R/B, 63525

Orbit data source: Space-Track

CZ-3B R/B, 63525 is space debris in HEO originally from a launch on Thu, 10 Apr 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.

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Identifier
63525, 2025-073B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-04-10 (5 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: 1 week ago

TLE from 1 week ago
0 CZ-3B R/B
1 63525U 25073B   25252.24523258  .00303254  10083-7  21747-2 0  9994
2 63525  19.3986  20.1846 6796593 305.1118   8.8577  2.98426021  3804
Epoch: 2025-09-09T05:53Z
TLE epoch observation values (Epoch: 2025-09-09T05:53:08.094Z)
Latitude
-0.00111°
Longitude
-56.6295°
Altitude
1,489.902 km
Speed
9.042 km/s
True Right ascension
01h 20m 46s
True Declination
0° 00' 04"
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
10:22:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
27,858.905 km
Perigee altitude
151.472 km
Semi-major axis
20,383.325 km
Eccentricity
0.67966
Inclination
19.3986°
RAAN
20.1846°
Arg. of periapsis
305.1118°
True anomaly
55.37954°
Mean anomaly
8.8577°
Eccentric anomaly
25.81623°
Mean motion
0.74581 °/min
Orbital period
482.69 mins
BSTAR
0.0021747
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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