Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
Latest
Satellite identification and parameters
Extended collection of information and parameters for FENGYUN 1C DEB.
Object identification
Identified? True
Debris? True
Object name: FENGYUN 1C DEB
International designator: 1999-025CYV
Object number (NORAD): 32352
Object ID (CCSDS): 32352
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.933 minutes
Inclination: 98.7764 deg
SMA: 7133.452 km
Apoapsis: 842.904 km
Periapsis: 667.73 km
RAAN: 84.2869 deg
Eccentricy: 0.0122784
Argument of periapsis: 341.2779 deg
Mean anomaly: 18.3913 deg
Mean motion: 14.40964077 rev/day
Mean motion (dot): 0.00000744 rev/day2
B* drag term: 0.00022659 1/REarth
Two-line elements (TLE)
Creation date: June 18, 2025, 5:28 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 17, 2025, 11:40 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32352U 99025CYV 25168.98619996 .00000744 00000-0 22659-3 0 9991
TLE line 2: 2 32352 98.7764 84.2869 0122784 341.2779 18.3913 14.40964077627093
Live tracking on map
Real-time ground track for satellite FENGYUN 1C DEB.
Associated space launch
Chinese polar orbiting meteorological satellite
FENGYUN 1C DEB was lifted into orbit during the mission ‘Long March 4B | Feng Yun 1C’, on board a Long March 4B space rocket.
The launch took place on May 10, 1999, 1:33 a.m. from Launch Complex 7.
For more information about the launch, click the button.
Long March 4B | Feng Yun 1C
Agency: N/A
Status: Launch Successful
Launch date: May 10, 1999, 1:33 a.m. UTC
Rocket: Long March 4B
Launch pad: Launch Complex 7
Location: Taiyuan Satellite Launch Center, People's Republic of China
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