Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9500
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025CVQ
Object number (NORAD): 32218
Object ID (CCSDS): 32218
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.044 minutes
Inclination: 98.8155 deg
SMA: 7091.071 km
Apoapsis: 758.329 km
Periapsis: 667.543 km
RAAN: 313.5346 deg
Eccentricy: 0.0064014
Argument of periapsis: 3.1348 deg
Mean anomaly: 169.7079 deg
Mean motion: 14.53901523 rev/day
Mean motion (dot): 0.00003943 rev/day2
B* drag term: 0.00092426 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 7:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 11, 2025, 7:02 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32218U 99025CVQ 25131.29315172 .00003943 00000-0 92426-3 0 9998
TLE line 2: 2 32218 98.8155 313.5346 0064014 3.1348 169.7079 14.53901523932560
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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