Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025BGC
Object number (NORAD): 31082
Object ID (CCSDS): 31082
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.945 minutes
Inclination: 98.6763 deg
SMA: 7228.869 km
Apoapsis: 902.209 km
Periapsis: 799.259 km
RAAN: 136.6816 deg
Eccentricy: 0.0071208
Argument of periapsis: 119.8874 deg
Mean anomaly: 240.9398 deg
Mean motion: 14.1252854 rev/day
Mean motion (dot): 0.00002174 rev/day2
B* drag term: 0.0011702 1/REarth
Two-line elements (TLE)
Creation date: May 2, 2025, 3:16 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 2, 2025, 6:29 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31082U 99025BGC 25122.27047913 .00002174 00000-0 11702-2 0 9991
TLE line 2: 2 31082 98.6763 136.6816 0071208 119.8874 240.9398 14.12528540931406
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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