Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9615
Days in orbit
Revolutions
≈ 14.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025CHJ
Object number (NORAD): 31820
Object ID (CCSDS): 31820
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 96.783 minutes
Inclination: 98.9575 deg
SMA: 6982.747 km
Apoapsis: 716.664 km
Periapsis: 492.56 km
RAAN: 44.8308 deg
Eccentricy: 0.01604703
Argument of periapsis: 330.5401 deg
Mean anomaly: 28.6839 deg
Mean motion: 14.87864217 rev/day
Mean motion (dot): 0.00012103 rev/day2
B* drag term: 0.0010477166 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 3:39 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31820U 99025CHJ 25247.15260569 .00012103 00000-0 10477-2 0 9991
TLE line 2: 2 31820 98.9575 44.8308 0160470 330.5401 28.6839 14.87864217967736
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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