Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9659
Days in orbit
Revolutions
≈ 14.5
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: 1999-025CCE
Object number (NORAD): 31672
Object ID (CCSDS): 31672
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.323 minutes
Inclination: 98.9609 deg
SMA: 7104.384 km
Apoapsis: 803.874 km
Periapsis: 648.624 km
RAAN: 114.2476 deg
Eccentricy: 0.0109263
Argument of periapsis: 151.5196 deg
Mean anomaly: 209.2026 deg
Mean motion: 14.49816808 rev/day
Mean motion (dot): 0.0001183 rev/day2
B* drag term: 0.0028493 1/REarth
Two-line elements (TLE)
Creation date: Oct. 17, 2025, 8:16 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 17, 2025, 6:03 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31672U 99025CCE 25290.25218804 .00011830 00000-0 28493-2 0 9993
TLE line 2: 2 31672 98.9609 114.2476 0109263 151.5196 209.2026 14.49816808640523
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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