Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 14.2
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: 1999-025CVV
Object number (NORAD): 32223
Object ID (CCSDS): 32223
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.428 minutes
Inclination: 98.8455 deg
SMA: 7204.414 km
Apoapsis: 862.075 km
Periapsis: 790.483 km
RAAN: 262.5914 deg
Eccentricy: 0.0049686
Argument of periapsis: 69.5975 deg
Mean anomaly: 351.448 deg
Mean motion: 14.19726766 rev/day
Mean motion (dot): 0.00001859 rev/day2
B* drag term: 0.00088862 1/REarth
Two-line elements (TLE)
Creation date: July 2, 2025, 5:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 10:42 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32223U 99025CVV 25183.44624021 .00001859 00000-0 88862-3 0 9997
TLE line 2: 2 32223 98.8455 262.5914 0049686 69.5975 351.4480 14.19726766619062
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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