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 (6 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: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 63525U 25073B   25294.18617799  .00141212  35806-6  17590-2 0  9991
2 63525  19.3778 355.6720 6643667 350.0020   1.6578  3.19294740  5094
Epoch: 2025-10-21T04:28Z
TLE epoch observation values (Epoch: 2025-10-21T04:28:05.778Z)
Latitude
-0.0001°
Longitude
-101.23099°
Altitude
196.203 km
Speed
10.039 km/s
True Right ascension
23h 42m 41s
True Declination
0° 00' 00"
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
00:21:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
26,052.644 km
Perigee altitude
161.798 km
Semi-major axis
19,485.358 km
Eccentricity
0.66437
Inclination
19.3778°
RAAN
355.672°
Arg. of periapsis
350.002°
True anomaly
10.94574°
Mean anomaly
1.6578°
Eccentric anomaly
4.9273°
Mean motion
0.79796 °/min
Orbital period
451.15 mins
BSTAR
0.001759
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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