Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9609
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.6
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: 1999-025BCS
Object number (NORAD): 31000
Object ID (CCSDS): 31000
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.177 minutes
Inclination: 97.5802 deg
SMA: 7239.841 km
Apoapsis: 981.254 km
Periapsis: 742.158 km
RAAN: 287.07 deg
Eccentricy: 0.0165125
Argument of periapsis: 12.8842 deg
Mean anomaly: 165.2066 deg
Mean motion: 14.09318733 rev/day
Mean motion (dot): 0.00001255 rev/day2
B* drag term: 0.00065200388 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 8:56 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31000U 99025BCS 25241.87242637 .00001255 00000-0 65200-3 0 9991
TLE line 2: 2 31000 97.5802 287.0700 0165125 12.8842 165.2066 14.09318733684795
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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