Key statistics
Satellite CZ-4C DEB at a glance.
Uptime
4367
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4C DEB.
Object identification
Identified? True
Debris? True
Object name: CZ-4C DEB
International designator: 2013-052E
Object number (NORAD): 43410
Object ID (CCSDS): 43410
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.637 minutes
Inclination: 98.7845 deg
SMA: 7355.583 km
Apoapsis: 1156.912 km
Periapsis: 797.983 km
RAAN: 46.76 deg
Eccentricy: 0.02439837
Argument of periapsis: 91.8798 deg
Mean anomaly: 271.0313 deg
Mean motion: 13.7618602 rev/day
Mean motion (dot): 0.00000723 rev/day2
B* drag term: 0.00062744696 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 4:29 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 4:41 p.m. UTC
TLE line 0: 0 CZ-4C DEB
TLE line 1: 1 43410U 13052E 25246.69561077 .00000723 00000-0 62745-3 0 9992
TLE line 2: 2 43410 98.7845 46.7600 0243984 91.8798 271.0313 13.76186020591129
Live tracking on map
Real-time ground track for satellite CZ-4C DEB.
Associated space launch
CZ-4C DEB was lifted into orbit during the mission ‘Long March 4C | Fengyun-3C’, on board a Long March 4C space rocket.
The launch took place on Sept. 23, 2013, 3:07 a.m. from Launch Complex 9.
For more information about the launch, click the button.

Long March 4C | Fengyun-3C
Agency: N/A
Status: Launch Successful
Launch date: Sept. 23, 2013, 3:07 a.m. UTC
Rocket: Long March 4C
Launch pad: Launch Complex 9
Location: Taiyuan Satellite Launch Center, People's Republic of China
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