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 (1 year 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   26072.59700012  .00118252  10978-6  26449-2 0  9993
2 63362  26.9496 258.1049 6784136  88.7938 341.7704  2.98634236  9496
Epoch: 2026-03-13T14:19Z
TLE epoch observation values (Epoch: 2026-03-13T14:19:40.810Z)
Latitude
-0.00046°
Longitude
-128.07188°
Altitude
4,436.198 km
Speed
7.358 km/s
True Right ascension
17h 12m 18s
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
04:09:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
27,816.275 km
Perigee altitude
173.56 km
Semi-major axis
20,373.055 km
Eccentricity
0.67841
Inclination
26.9496°
RAAN
258.1049°
Arg. of periapsis
88.7938°
True anomaly
271.26286°
Mean anomaly
341.7704°
Eccentric anomaly
313.64073°
Mean motion
0.74638 °/min
Orbital period
482.33 mins
BSTAR
0.0026449
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Other satellites on launch #62 in the year 2025 (2025-03-26 UTC)

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