Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025CXF
Object number (NORAD): 32314
Object ID (CCSDS): 32314
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.339 minutes
Inclination: 98.8627 deg
SMA: 7009.487 km
Apoapsis: 736.067 km
Periapsis: 526.636 km
RAAN: 88.2704 deg
Eccentricy: 0.0149391
Argument of periapsis: 167.7932 deg
Mean anomaly: 192.6962 deg
Mean motion: 14.79358552 rev/day
Mean motion (dot): 0.00020854 rev/day2
B* drag term: 0.0023179 1/REarth
Two-line elements (TLE)
Creation date: Dec. 9, 2025, 11:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 9, 2025, 1:16 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32314U 99025CXF 25343.55282576 .00020854 00000-0 23179-2 0 9998
TLE line 2: 2 32314 98.8627 88.2704 0149391 167.7932 192.6962 14.79358552973830
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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