Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025CYF
Object number (NORAD): 32338
Object ID (CCSDS): 32338
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.66 minutes
Inclination: 98.9062 deg
SMA: 7120.426 km
Apoapsis: 785.511 km
Periapsis: 699.071 km
RAAN: 173.9743 deg
Eccentricy: 0.00606985
Argument of periapsis: 68.907 deg
Mean anomaly: 291.8595 deg
Mean motion: 14.44919898 rev/day
Mean motion (dot): 0.00018733 rev/day2
B* drag term: 0.0052572846 1/REarth
Two-line elements (TLE)
Creation date: Nov. 1, 2025, 7:40 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Nov. 6, 2024, 8:49 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32338U 99025CYF 24311.36798734 .00018733 00000-0 52573-2 0 9998
TLE line 2: 2 32338 98.9062 173.9743 0060698 68.9070 291.8595 14.44919898593258
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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