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 (9 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 8.0 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 63362U 25062B   25348.18487876  .00060212 -18344-6  14898-2 0  9996
2 63362  27.1519 303.4845 6923898  13.6861 358.0948  2.79385956  6922
Epoch: 2025-12-14T04:26Z
TLE epoch observation values (Epoch: 2025-12-14T04:26:13.524Z)
Latitude
0.00059°
Longitude
153.82453°
Altitude
257.875 km
Speed
10.07 km/s
True Right ascension
20h 13m 55s
True Declination
0° 00' 02"
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
05:57:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
29,666.723 km
Perigee altitude
173.407 km
Semi-major axis
21,298.202 km
Eccentricity
0.69239
Inclination
27.1519°
RAAN
303.4845°
Arg. of periapsis
13.6861°
True anomaly
345.5977°
Mean anomaly
358.0948°
Eccentric anomaly
353.83323°
Mean motion
0.69828 °/min
Orbital period
515.55 mins
BSTAR
0.0014898
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Other satellites on launch #62 in the year 2025 (2025-03-26 UTC)

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