CZ-2C R/B, 55846

Orbit data source: Space-Track

CZ-2C R/B, 55846 is space debris in SSO originally from a launch on Mon, 13 Mar 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
55846, 2023-032C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
2023-03-13 (3 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.7 m
Radar Cross Section
23.715 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-2C R/B
1 55846U 23032C   26171.41829558  .00010876  00000-0  24006-3 0  9994
2 55846  97.5797 279.8239 0031116   6.1210 354.0411 15.43547852182199
Epoch: 2026-06-20T10:02Z
TLE epoch observation values (Epoch: 2026-06-20T10:02:20.738Z)
Latitude
-0.00002°
Longitude
-139.39571°
Altitude
417.674 km
Speed
7.672 km/s
True Right ascension
18h 39m 17s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
21:35:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.783 km
Perigee altitude
411.398 km
Semi-major axis
6,810.727 km
Eccentricity
0.00311
Inclination
97.5797°
RAAN
279.8239°
Arg. of periapsis
6.121°
True anomaly
354.00394°
Mean anomaly
354.0411°
Eccentric anomaly
354.02253°
Mean motion
3.86147 °/min
Orbital period
93.23 mins
BSTAR
0.00024006
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