Key statistics
Satellite CZ-4C DEB at a glance.
Uptime
4368
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 2013-052C
Object number (NORAD): 43408
Object ID (CCSDS): 43408
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.224 minutes
Inclination: 98.7075 deg
SMA: 7336.191 km
Apoapsis: 1117.715 km
Periapsis: 798.398 km
RAAN: 54.6961 deg
Eccentricy: 0.02176314
Argument of periapsis: 314.5586 deg
Mean anomaly: 43.7977 deg
Mean motion: 13.81646038 rev/day
Mean motion (dot): 0.00000356 rev/day2
B* drag term: 0.0003110601 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 3:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 5:44 p.m. UTC
TLE line 0: 0 CZ-4C DEB
TLE line 1: 1 43408U 13052C 25250.73946533 .00000356 00000-0 31106-3 0 9992
TLE line 2: 2 43408 98.7075 54.6961 0217631 314.5586 43.7977 13.81646038594005
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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