CZ-3B R/B, 63362

Orbit data source: Space-Track

CZ-3B R/B, 63362 is space debris in HEO originally from a launch on Wed, 26 Mar 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
63362, 2025-062B
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)
2025-03-26 (6 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 CZ-3B R/B
1 63362U 25062B   25255.27874978  .00025421  27086-6  74174-3 0  9995
2 63362  27.3603 347.1365 6973432 301.1597   8.9353  2.72483946  4368
Epoch: 2025-09-12T06:41Z
TLE epoch observation values (Epoch: 2025-09-12T06:41:23.98Z)
Latitude
-0.00013°
Longitude
-104.73562°
Altitude
1,809.99 km
Speed
8.885 km/s
True Right ascension
23h 08m 34s
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
23:53:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,380.003 km
Perigee altitude
176.283 km
Semi-major axis
21,656.28 km
Eccentricity
0.69734
Inclination
27.3603°
RAAN
347.1365°
Arg. of periapsis
301.1597°
True anomaly
59.61107°
Mean anomaly
8.9353°
Eccentric anomaly
27.19623°
Mean motion
0.68103 °/min
Orbital period
528.61 mins
BSTAR
0.00074174
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Other satellites on launch #62 in the year 2025 (2025-03-26 UTC)

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