Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
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: 1999-025BVA
Object number (NORAD): 31462
Object ID (CCSDS): 31462
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.91 minutes
Inclination: 98.6905 deg
SMA: 7227.241 km
Apoapsis: 872.209 km
Periapsis: 826.002 km
RAAN: 2.814 deg
Eccentricy: 0.00319673
Argument of periapsis: 211.2699 deg
Mean anomaly: 163.3139 deg
Mean motion: 14.13005923 rev/day
Mean motion (dot): 0.00000874 rev/day2
B* drag term: 0.00048932304 1/REarth
Two-line elements (TLE)
Creation date: Dec. 10, 2025, 7:58 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 10, 2025, 8:12 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31462U 99025BVA 25344.34197066 .00000874 00000-0 48932-3 0 9993
TLE line 2: 2 31462 98.6905 2.8140 0031967 211.2699 163.3139 14.13005923958226
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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