Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.9
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: 1999-025CDX
Object number (NORAD): 31724
Object ID (CCSDS): 31724
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.373 minutes
Inclination: 97.8558 deg
SMA: 7106.754 km
Apoapsis: 836.431 km
Periapsis: 620.807 km
RAAN: 352.7338 deg
Eccentricy: 0.01517036
Argument of periapsis: 242.0652 deg
Mean anomaly: 116.5116 deg
Mean motion: 14.49091574 rev/day
Mean motion (dot): 0.00013613 rev/day2
B* drag term: 0.0030997985 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 4:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 6:08 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31724U 99025CDX 25346.75555925 .00013613 00000-0 30998-2 0 9990
TLE line 2: 2 31724 97.8558 352.7338 0151704 242.0652 116.5116 14.49091574644921
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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