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 (1 year ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 5.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 63525U 25073B   26126.73572230  .00164878  21765-6  87476-3 0  9990
2 63525  19.2077 229.0166 6438910 221.4326  65.8175  3.49820943 11709
Epoch: 2026-05-06T17:39Z
TLE epoch observation values (Epoch: 2026-05-06T17:39:26.406Z)
Latitude
0.00015°
Longitude
99.61212°
Altitude
14,398.648 km
Speed
4.077 km/s
True Right ascension
15h 16m 15s
True Declination
0° 00' 01"
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
11:45:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,762.405 km
Perigee altitude
151.078 km
Semi-major axis
18,334.878 km
Eccentricity
0.64389
Inclination
19.2077°
RAAN
229.0166°
Arg. of periapsis
221.4326°
True anomaly
138.63987°
Mean anomaly
65.8175°
Eccentric anomaly
101.9149°
Mean motion
0.87423 °/min
Orbital period
411.79 mins
BSTAR
0.00087476
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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