CZ-7A R/B, 55132

Orbit data source: Space-Track

CZ-7A R/B, 55132 is space debris in HEO originally from a launch on Sun, 08 Jan 2023 UTC launched from the Wenchang Satellite Launch Center (WSC). 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
55132, 2023-002B
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)
2023-01-08 (3 years ago)
Launch vehicle
Unknown
Launch site
Wenchang Satellite Launch Center (WSC)
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: 1 day ago

TLE from 1 day ago
0 CZ-7A R/B
1 55132U 23002B   25260.16357250  .00029982  00000-0  11427-2 0  9994
2 55132  16.4570 196.2757 5882161 266.0502  28.9370  4.29147636 31926
Epoch: 2025-09-17T03:55Z
TLE epoch observation values (Epoch: 2025-09-17T03:55:32.663Z)
Latitude
-0°
Longitude
140.99551°
Altitude
4,523.163 km
Speed
6.943 km/s
True Right ascension
13h 04m 54s
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
02:26:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,033.436 km
Perigee altitude
210.435 km
Semi-major axis
16,000.073 km
Eccentricity
0.58822
Inclination
16.457°
RAAN
196.2757°
Arg. of periapsis
266.0502°
True anomaly
94.02879°
Mean anomaly
28.937°
Eccentric anomaly
57.29685°
Mean motion
1.07241 °/min
Orbital period
335.69 mins
BSTAR
0.0011427
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Other satellites on launch #2 in the year 2023 (2023-01-08 UTC)

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