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: 15 hours ago

TLE from 15 hours ago
0 CZ-3B R/B
1 63525U 25073B   26177.24628747  .00240292 -29543-6  67193-3 0  9999
2 63525  19.2042 192.8009 6295114 287.4378  16.0487  3.71801102 13527
Epoch: 2026-06-26T05:54Z
TLE epoch observation values (Epoch: 2026-06-26T05:54:39.237Z)
Latitude
-0.00011°
Longitude
-170.18269°
Altitude
2,567.559 km
Speed
8.152 km/s
True Right ascension
12h 51m 26s
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
08:04:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
22,309.581 km
Perigee altitude
144.353 km
Semi-major axis
17,605.104 km
Eccentricity
0.62951
Inclination
19.2042°
RAAN
192.8009°
Arg. of periapsis
287.4378°
True anomaly
72.44177°
Mean anomaly
16.0487°
Eccentric anomaly
38.5035°
Mean motion
0.92915 °/min
Orbital period
387.45 mins
BSTAR
0.00067193
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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