CZ-4C R/B, 57798

Orbit data source: Space-Track

CZ-4C R/B, 57798 is space debris in SSO originally from a launch on Wed, 06 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
57798, 2023-136B
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)
2023-09-06 (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 57798U 23136B   26171.44109242  .00001551  00000-0  10561-3 0  9992
2 57798  98.3082 166.8393 0107321 287.7110  71.2421 15.03538626152402
Epoch: 2026-06-20T10:35Z
TLE epoch observation values (Epoch: 2026-06-20T10:35:10.385Z)
Latitude
-0.00006°
Longitude
99.39036°
Altitude
535.821 km
Speed
7.607 km/s
True Right ascension
11h 07m 21s
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
21:23:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.409 km
Perigee altitude
478.637 km
Semi-major axis
6,931.16 km
Eccentricity
0.01073
Inclination
98.3082°
RAAN
166.8393°
Arg. of periapsis
287.711°
True anomaly
72.41155°
Mean anomaly
71.2421°
Eccentric anomaly
71.82633°
Mean motion
3.76127 °/min
Orbital period
95.71 mins
BSTAR
0.00010561
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Other satellites on launch #136 in the year 2023 (2023-09-06 UTC)

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