CZ-4C R/B, 57655

Orbit data source: Space-Track

CZ-4C R/B, 57655 is space debris in SSO originally from a launch on Sun, 20 Aug 2023 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
57655, 2023-123B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2023-08-20 (3 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.5 m
Radar Cross Section
14.536 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-4C R/B
1 57655U 23123B   26171.42921058  .00012556  00000-0  30387-3 0  9990
2 57655  97.9722 162.0108 0058691  64.0981 296.6297 15.39459810157572
Epoch: 2026-06-20T10:18Z
TLE epoch observation values (Epoch: 2026-06-20T10:18:03.794Z)
Latitude
0.00003°
Longitude
98.85103°
Altitude
433.034 km
Speed
7.662 km/s
True Right ascension
10h 48m 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
21:40:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.714 km
Perigee altitude
404.627 km
Semi-major axis
6,822.808 km
Eccentricity
0.00587
Inclination
97.9722°
RAAN
162.0108°
Arg. of periapsis
64.0981°
True anomaly
296.02652°
Mean anomaly
296.6297°
Eccentric anomaly
296.32831°
Mean motion
3.85122 °/min
Orbital period
93.48 mins
BSTAR
0.00030387
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Other satellites on launch #123 in the year 2023 (2023-08-20 UTC)

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