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: 17 hours ago

TLE from 17 hours ago
0 CZ-2C R/B
1 55846U 23032C   25306.29471880  .00015586  00000-0  44223-3 0  9996
2 55846  97.5790  41.7023 0038947 109.5237 251.0218 15.35534998146789
Epoch: 2025-11-02T07:04Z
TLE epoch observation values (Epoch: 2025-11-02T07:04:23.704Z)
Latitude
-0.0001°
Longitude
-106.20896°
Altitude
471.193 km
Speed
7.626 km/s
True Right ascension
02h 46m 48s
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
20:20:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.903 km
Perigee altitude
429.666 km
Semi-major axis
6,834.421 km
Eccentricity
0.00389
Inclination
97.579°
RAAN
41.7023°
Arg. of periapsis
109.5237°
True anomaly
250.60043°
Mean anomaly
251.0218°
Eccentric anomaly
250.81105°
Mean motion
3.84141 °/min
Orbital period
93.72 mins
BSTAR
0.00044223
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