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: 20 hours ago

TLE from 20 hours ago
0 CZ-3B R/B
1 63525U 25073B   26096.45423239  .00119419  55175-6  15513-2 0  9994
2 63525  19.2553 249.5001 6481551 184.0964 165.5333  3.42410165 10655
Epoch: 2026-04-06T10:54Z
TLE epoch observation values (Epoch: 2026-04-06T10:54:05.678Z)
Latitude
0.00001°
Longitude
-108.7853°
Altitude
24,119.152 km
Speed
2.169 km/s
True Right ascension
16h 37m 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
12:44:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
24,274.93 km
Perigee altitude
165.619 km
Semi-major axis
18,598.412 km
Eccentricity
0.64816
Inclination
19.2553°
RAAN
249.5001°
Arg. of periapsis
184.0964°
True anomaly
175.93193°
Mean anomaly
165.5333°
Eccentric anomaly
171.20894°
Mean motion
0.85572 °/min
Orbital period
420.7 mins
BSTAR
0.0015513
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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

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