Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.6
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: 1999-025CVJ
Object number (NORAD): 32212
Object ID (CCSDS): 32212
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.036 minutes
Inclination: 99.5794 deg
SMA: 7138.365 km
Apoapsis: 859.27 km
Periapsis: 661.189 km
RAAN: 194.5061 deg
Eccentricy: 0.0138744
Argument of periapsis: 4.2153 deg
Mean anomaly: 175.4777 deg
Mean motion: 14.39476826 rev/day
Mean motion (dot): 0.00001923 rev/day2
B* drag term: 0.00056822 1/REarth
Two-line elements (TLE)
Creation date: May 4, 2025, 6:56 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 3, 2025, 10:47 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32212U 99025CVJ 25123.94965277 .00001923 00000-0 56822-3 0 9998
TLE line 2: 2 32212 99.5794 194.5061 0138744 4.2153 175.4777 14.39476826929045
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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