Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
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: 99.68 minutes
Inclination: 98.9046 deg
SMA: 7121.391 km
Apoapsis: 788.321 km
Periapsis: 698.19 km
RAAN: 166.1342 deg
Eccentricy: 0.0063282
Argument of periapsis: 90.0523 deg
Mean anomaly: 270.7918 deg
Mean motion: 14.44626397 rev/day
Mean motion (dot): 0.0001741 rev/day2
B* drag term: 0.0049083 1/REarth
Two-line elements (TLE)
Creation date: May 2, 2025, 2:33 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 29, 2024, 9:19 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32338U 99025CYF 24303.88847571 .00017410 00000-0 49083-2 0 9993
TLE line 2: 2 32338 98.9046 166.1342 0063282 90.0523 270.7918 14.44626397592174
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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