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: 5 days ago

TLE from 5 days ago
0 CZ-3B R/B
1 63525U 25073B   26154.59098799  .00224762  21905-6  61834-3 0  9993
2 63525  19.1963 209.4046 6369765 257.1536  29.1720  3.60695775 12695
Epoch: 2026-06-03T14:11Z
TLE epoch observation values (Epoch: 2026-06-03T14:11:01.362Z)
Latitude
-0.00003°
Longitude
104.68171°
Altitude
6,073.828 km
Speed
6.467 km/s
True Right ascension
13h 57m 56s
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
03:14:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,029.422 km
Perigee altitude
143.42 km
Semi-major axis
17,964.558 km
Eccentricity
0.63698
Inclination
19.1963°
RAAN
209.4046°
Arg. of periapsis
257.1536°
True anomaly
102.86647°
Mean anomaly
29.172°
Eccentric anomaly
61.13324°
Mean motion
0.9014 °/min
Orbital period
399.38 mins
BSTAR
0.00061834
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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