CZ-3B R/B, 56565

Orbit data source: Space-Track

CZ-3B R/B, 56565 is space debris in HEO originally from a launch on Wed, 17 May 2023 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
56565, 2023-066B
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)
2023-05-17 (3 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 56565U 23066B   26162.27779528  .00308047 -43105-6  11007-2 0  9991
2 56565  28.1281 125.9509 4967670 157.4362 235.5826  5.86915908 44942
Epoch: 2026-06-11T06:40Z
TLE epoch observation values (Epoch: 2026-06-11T06:40:01.512Z)
Latitude
0.00001°
Longitude
126.31367°
Altitude
11,681.798 km
Speed
3.667 km/s
True Right ascension
08h 23m 46s
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
16:28:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
13,058.515 km
Perigee altitude
156.724 km
Semi-major axis
12,985.756 km
Eccentricity
0.49677
Inclination
28.1281°
RAAN
125.9509°
Arg. of periapsis
157.4362°
True anomaly
202.60836°
Mean anomaly
235.5826°
Eccentric anomaly
218.04258°
Mean motion
1.4667 °/min
Orbital period
245.45 mins
BSTAR
0.0011007
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Other satellites on launch #66 in the year 2023 (2023-05-17 UTC)

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