Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9669
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.4
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: 1999-025CJF
Object number (NORAD): 31841
Object ID (CCSDS): 31841
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.626 minutes
Inclination: 98.4194 deg
SMA: 7261.011 km
Apoapsis: 1108.4 km
Periapsis: 657.353 km
RAAN: 111.4396 deg
Eccentricy: 0.0310595
Argument of periapsis: 79.9004 deg
Mean anomaly: 94.0326 deg
Mean motion: 14.03159638 rev/day
Mean motion (dot): 0.00003453 rev/day2
B* drag term: 0.0014624 1/REarth
Two-line elements (TLE)
Creation date: Oct. 26, 2025, 2:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 26, 2025, 6:24 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31841U 99025CJF 25299.26703046 .00003453 00000-0 14624-2 0 9991
TLE line 2: 2 31841 98.4194 111.4396 0310595 79.9004 94.0326 14.03159638586734
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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