Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 15.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025BRA
Object number (NORAD): 31346
Object ID (CCSDS): 31346
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 95.303 minutes
Inclination: 98.8654 deg
SMA: 6911.361 km
Apoapsis: 609.671 km
Periapsis: 456.781 km
RAAN: 314.4394 deg
Eccentricy: 0.01106077
Argument of periapsis: 13.5681 deg
Mean anomaly: 346.8476 deg
Mean motion: 15.10975251 rev/day
Mean motion (dot): 0.00036896 rev/day2
B* drag term: 0.001904937 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 8:59 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31346U 99025BRA 25347.37499314 .00036896 00000-0 19049-2 0 9990
TLE line 2: 2 31346 98.8654 314.4394 0110608 13.5681 346.8476 15.10975251995059
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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