Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.8
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: 1999-025CDU
Object number (NORAD): 31721
Object ID (CCSDS): 31721
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.851 minutes
Inclination: 99.7565 deg
SMA: 7365.586 km
Apoapsis: 1223.126 km
Periapsis: 751.776 km
RAAN: 101.0366 deg
Eccentricy: 0.0319968
Argument of periapsis: 32.9274 deg
Mean anomaly: 117.4625 deg
Mean motion: 13.73383513 rev/day
Mean motion (dot): 0.0000142 rev/day2
B* drag term: 0.0010908 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 9:41 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31721U 99025CDU 25126.40358812 .00001420 00000-0 10908-2 0 9993
TLE line 2: 2 31721 99.7565 101.0366 0319968 32.9274 117.4625 13.73383513643610
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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