Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 13.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.4
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: 1999-025CVF
Object number (NORAD): 32209
Object ID (CCSDS): 32209
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 106.945 minutes
Inclination: 99.4083 deg
SMA: 7463.331 km
Apoapsis: 1331.705 km
Periapsis: 838.686 km
RAAN: 88.4775 deg
Eccentricy: 0.0330294
Argument of periapsis: 210.6681 deg
Mean anomaly: 147.4775 deg
Mean motion: 13.4649186 rev/day
Mean motion (dot): 0.00001256 rev/day2
B* drag term: 0.0015477 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 8:01 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32209U 99025CVF 25128.33425076 .00001256 00000-0 15477-2 0 9999
TLE line 2: 2 32209 99.4083 88.4775 0330294 210.6681 147.4775 13.46491860870366
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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