Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.3
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: 1999-025CNG
Object number (NORAD): 31955
Object ID (CCSDS): 31955
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.366 minutes
Inclination: 99.2809 deg
SMA: 7058.687 km
Apoapsis: 711.078 km
Periapsis: 650.027 km
RAAN: 224.5542 deg
Eccentricy: 0.00432453
Argument of periapsis: 178.1846 deg
Mean anomaly: 239.4777 deg
Mean motion: 14.63918343 rev/day
Mean motion (dot): 0.00010824 rev/day2
B* drag term: 0.0020497321 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 3:10 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31955U 99025CNG 25347.63245756 .00010824 00000-0 20497-2 0 9996
TLE line 2: 2 31955 99.2809 224.5542 0043245 178.1846 239.4777 14.63918343965707
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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