Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
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: 97.59 minutes
Inclination: 98.8632 deg
SMA: 7021.506 km
Apoapsis: 753.771 km
Periapsis: 532.971 km
RAAN: 273.5733 deg
Eccentricy: 0.0157231
Argument of periapsis: 308.3218 deg
Mean anomaly: 50.394 deg
Mean motion: 14.75561687 rev/day
Mean motion (dot): 0.00003404 rev/day2
B* drag term: 0.00041712 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 5:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 11:59 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32314U 99025CXF 25184.49991134 .00003404 00000-0 41712-3 0 9997
TLE line 2: 2 32314 98.8632 273.5733 0157231 308.3218 50.3940 14.75561687950358
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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