CZ-4C R/B, 57959

Orbit data source: Space-Track

CZ-4C R/B, 57959 is space debris in SSO originally from a launch on Tue, 26 Sep 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
57959, 2023-149B
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)
2023-09-26 (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 57959U 23149B   26171.45008590  .00001945  00000-0  14620-3 0  9997
2 57959  98.1843 180.2934 0107702   0.5019 359.6292 14.99410092149097
Epoch: 2026-06-20T10:48Z
TLE epoch observation values (Epoch: 2026-06-20T10:48:07.421Z)
Latitude
0.00002°
Longitude
109.59794°
Altitude
496.924 km
Speed
7.657 km/s
True Right ascension
12h 01m 10s
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
21:30:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.532 km
Perigee altitude
490.958 km
Semi-major axis
6,943.882 km
Eccentricity
0.01077
Inclination
98.1843°
RAAN
180.2934°
Arg. of periapsis
0.5019°
True anomaly
359.6211°
Mean anomaly
359.6292°
Eccentric anomaly
359.62516°
Mean motion
3.75094 °/min
Orbital period
95.98 mins
BSTAR
0.0001462
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Other satellites on launch #149 in the year 2023 (2023-09-26 UTC)

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