Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.5
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: 1999-025BQV
Object number (NORAD): 31341
Object ID (CCSDS): 31341
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.221 minutes
Inclination: 99.565 deg
SMA: 7099.527 km
Apoapsis: 762.105 km
Periapsis: 680.678 km
RAAN: 206.2272 deg
Eccentricy: 0.0057347
Argument of periapsis: 98.7923 deg
Mean anomaly: 292.4714 deg
Mean motion: 14.51304968 rev/day
Mean motion (dot): 0.00004082 rev/day2
B* drag term: 0.0010177 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 11:55 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31341U 99025BQV 25186.99654562 .00004082 00000-0 10177-2 0 9997
TLE line 2: 2 31341 99.5650 206.2272 0057347 98.7923 292.4714 14.51304968953000
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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