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 (8 months 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: 14 hours ago

TLE from 14 hours ago
0 CZ-3B R/B
1 63525U 25073B   25342.49161350  .00055477 -84033-7  12069-2 0  9997
2 63525  19.3408 325.7811 6567281  44.6687 352.4823  3.29073181  6664
Epoch: 2025-12-08T11:47Z
TLE epoch observation values (Epoch: 2025-12-08T11:47:55.406Z)
Latitude
0.00011°
Longitude
71.30464°
Altitude
1,032.528 km
Speed
9.311 km/s
True Right ascension
21h 43m 06s
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
00:24:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,261.19 km
Perigee altitude
177.49 km
Semi-major axis
19,097.477 km
Eccentricity
0.65673
Inclination
19.3408°
RAAN
325.7811°
Arg. of periapsis
44.6687°
True anomaly
315.67938°
Mean anomaly
352.4823°
Eccentric anomaly
338.99411°
Mean motion
0.82239 °/min
Orbital period
437.75 mins
BSTAR
0.0012069
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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