CZ-4C R/B, 52913

Orbit data source: Space-Track

CZ-4C R/B, 52913 is space debris in SSO originally from a launch on Mon, 27 Jun 2022 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
52913, 2022-069B
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)
2022-06-27 (4 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 52913U 22069B   26171.40242747  .00008100  00000-0  24219-3 0  9996
2 52913  98.0032 153.5163 0045262  87.4774 273.1647 15.33846576220523
Epoch: 2026-06-20T09:39Z
TLE epoch observation values (Epoch: 2026-06-20T09:39:29.733Z)
Latitude
-0.00005°
Longitude
100.02486°
Altitude
465.87 km
Speed
7.634 km/s
True Right ascension
10h 14m 03s
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
21:49:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.279 km
Perigee altitude
430.366 km
Semi-major axis
6,839.46 km
Eccentricity
0.00453
Inclination
98.0032°
RAAN
153.5163°
Arg. of periapsis
87.4774°
True anomaly
272.64667°
Mean anomaly
273.1647°
Eccentric anomaly
272.9057°
Mean motion
3.83717 °/min
Orbital period
93.82 mins
BSTAR
0.00024219
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Other satellites on launch #69 in the year 2022 (2022-06-27 UTC)

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