CZ-4B R/B, 43656

Orbit data source: Space-Track

CZ-4B R/B, 43656 is space debris in SSO originally from a launch on Wed, 24 Oct 2018 UTC via a CHANG ZHENG 4B launch vehicle from the Taiyaun Space Center, China (TSC). 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
43656, 2018-081B
Orbit
SSO
Last TLE update
13 hours ago
Origin
Flag of CNAliExpress, Alibaba Group (CN / PRC)
Manufacturer
SAST?
Mission
Commercial Communications
Bus & Motor
Unknown
Mass
1,020 kg wet, 20 kg dry
Launch date (UTC)
2018-10-24 (7 years ago)
Launch vehicle
CHANG ZHENG 4B
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.135 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 13 hours ago
0 CZ-4B R/B
1 43656U 18081B   25199.42625606  .00000066  00000-0  36528-4 0  9999
2 43656  99.3913  85.5248 0205726 147.6489 213.7502 14.31659245351541
Epoch: 2025-07-18T10:13Z
TLE epoch observation values (Epoch: 2025-07-18T10:13:48.523Z)
Latitude
-0.00003°
Longitude
-4.40526°
Altitude
912.587 km
Speed
7.332 km/s
True Right ascension
05h 42m 05s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-56.72845°
Longitude
10.70883°
Altitude
942.521 km
Speed
7.31 km/s
Apparent Right ascension
03h 00m 19s
Apparent Declination
-59° 57' 51"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:09:43
Azimuth
218.407° SW
Elevation
-56.915°
Doppler factor
1
Orbital elements
Apogee altitude
930.696 km
Perigee altitude
636.035 km
Semi-major axis
7,161.502 km
Eccentricity
0.02057
Inclination
99.3913°
RAAN
85.5248°
Arg. of periapsis
147.6489°
True anomaly
212.46801°
Mean anomaly
213.7502°
Eccentric anomaly
213.10639°
Mean motion
3.58127 °/min
Orbital period
100.52 mins
BSTAR
0.000036528
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