DECAYED

CZ-3B R/B, 62805 (Decayed)

Orbit data source: Space-Track

CZ-3B R/B, 62805 was space debris in LEO 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.

Not visible in the next 10 days
Identifier
62805, 2025-017B
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-01-23 (1 year 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: 1 week ago

TLE from 1 week ago
0 CZ-3B R/B
1 62805U 25017B   26092.89449087  .30516027 -18869-4  99190-3 0  9996
2 62805  27.9978 313.3941 1054618 113.8051 257.6571 14.05596359 18372
Epoch: 2026-04-02T21:28Z
TLE epoch observation values (Epoch: 2026-04-02T21:28:04.011Z)
Latitude
-0.00001°
Longitude
160.14095°
Altitude
1,110.172 km
Speed
7.179 km/s
True Right ascension
20h 53m 34s
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
19:35:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,643.931 km
Perigee altitude
113.31 km
Semi-major axis
7,256.757 km
Eccentricity
0.10546
Inclination
27.9978°
RAAN
313.3941°
Arg. of periapsis
113.8051°
True anomaly
246.25081°
Mean anomaly
257.6571°
Eccentric anomaly
251.91316°
Mean motion
3.51099 °/min
Orbital period
102.54 mins
BSTAR
0.0009919
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Other satellites on launch #17 in the year 2025 (2025-01-23 UTC)

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