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: 2 weeks ago

TLE from 2 weeks ago
0 CZ-3B R/B
1 63362U 25062B   26236.96037010  .00050735 -49246-6  84740-3 0  9998
2 63362  26.8413 168.1238 6675203 238.6969  39.7318  3.14309922 14578
Epoch: 2026-08-24T23:02Z
TLE epoch observation values (Epoch: 2026-08-24T23:02:55.976Z)
Latitude
0.00013°
Longitude
-150.86106°
Altitude
10,357.939 km
Speed
5.233 km/s
True Right ascension
11h 12m 25s
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
14:48:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
26,455.388 km
Perigee altitude
168.398 km
Semi-major axis
19,690.03 km
Eccentricity
0.66752
Inclination
26.8413°
RAAN
168.1238°
Arg. of periapsis
238.6969°
True anomaly
121.38132°
Mean anomaly
39.7318°
Eccentric anomaly
76.99724°
Mean motion
0.78555 °/min
Orbital period
458.28 mins
BSTAR
0.0008474
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Other satellites on launch #62 in the year 2025 (2025-03-26 UTC)

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