Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.5
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: 1999-025CPX
Object number (NORAD): 31994
Object ID (CCSDS): 31994
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.176 minutes
Inclination: 98.5314 deg
SMA: 7286.973 km
Apoapsis: 1026.111 km
Periapsis: 791.565 km
RAAN: 194.3896 deg
Eccentricy: 0.0160935
Argument of periapsis: 225.7408 deg
Mean anomaly: 133.0454 deg
Mean motion: 13.95667583 rev/day
Mean motion (dot): 0.00000352 rev/day2
B* drag term: 0.00025817 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 5:24 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31994U 99025CPX 25188.72533275 .00000352 00000-0 25817-3 0 9995
TLE line 2: 2 31994 98.5314 194.3896 0160935 225.7408 133.0454 13.95667583545928
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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