Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 14.2
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: 1999-025CVV
Object number (NORAD): 32223
Object ID (CCSDS): 32223
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.449 minutes
Inclination: 98.8435 deg
SMA: 7205.421 km
Apoapsis: 862.494 km
Periapsis: 792.077 km
RAAN: 206.692 deg
Eccentricy: 0.0048864
Argument of periapsis: 225.0214 deg
Mean anomaly: 203.477 deg
Mean motion: 14.19429292 rev/day
Mean motion (dot): 0.00003295 rev/day2
B* drag term: 0.0015682 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 11:38 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32223U 99025CVV 25127.48473698 .00003295 00000-0 15682-2 0 9996
TLE line 2: 2 32223 98.8435 206.6920 0048864 225.0214 203.4770 14.19429292611129
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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