Key statistics
Satellite CZ-4C DEB at a glance.
Uptime
4305
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: 104.642 minutes
Inclination: 98.7759 deg
SMA: 7355.799 km
Apoapsis: 1155.703 km
Periapsis: 799.625 km
RAAN: 350.446 deg
Eccentricy: 0.0242039
Argument of periapsis: 254.9139 deg
Mean anomaly: 102.5119 deg
Mean motion: 13.76125251 rev/day
Mean motion (dot): 0.00000307 rev/day2
B* drag term: 0.00028886 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 4:36 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 4:40 p.m. UTC
TLE line 0: 0 CZ-4C DEB
TLE line 1: 1 43410U 13052E 25185.69449961 .00000307 00000-0 28886-3 0 9997
TLE line 2: 2 43410 98.7759 350.4460 0242039 254.9139 102.5119 13.76125251582731
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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