CZ-3B R/B, 62805

Orbit data source: Space-Track

CZ-3B R/B, 62805 is space debris in HEO originally from a launch on Thu, 23 Jan 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
62805, 2025-017B
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)
2025-01-23 (9 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 4.5 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 CZ-3B R/B
1 62805U 25017B   25309.08609285  .00591553 -37753-7  74987-3 0  9992
2 62805  28.0584 203.7052 6423870  63.5492 347.3852  3.53642572  8533
Epoch: 2025-11-05T02:03Z
TLE epoch observation values (Epoch: 2025-11-05T02:03:58.422Z)
Latitude
0.0001°
Longitude
128.20522°
Altitude
1,922.147 km
Speed
8.61 km/s
True Right ascension
13h 35m 02s
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
12:11:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,516.066 km
Perigee altitude
131.02 km
Semi-major axis
18,201.68 km
Eccentricity
0.64239
Inclination
28.0584°
RAAN
203.7052°
Arg. of periapsis
63.5492°
True anomaly
296.41914°
Mean anomaly
347.3852°
Eccentric anomaly
327.73894°
Mean motion
0.88384 °/min
Orbital period
407.31 mins
BSTAR
0.00074987
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Other satellites on launch #17 in the year 2025 (2025-01-23 UTC)

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