Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 15.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025BZU
Object number (NORAD): 31614
Object ID (CCSDS): 31614
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 96.15 minutes
Inclination: 98.9762 deg
SMA: 6952.251 km
Apoapsis: 588.767 km
Periapsis: 559.465 km
RAAN: 253.6408 deg
Eccentricy: 0.00210739
Argument of periapsis: 3.2722 deg
Mean anomaly: 50.4872 deg
Mean motion: 14.97664823 rev/day
Mean motion (dot): 0.00087242 rev/day2
B* drag term: 0.007337979 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, 5:04 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31614U 99025BZU 25347.71118755 .00087242 00000-0 73380-2 0 9992
TLE line 2: 2 31614 98.9762 253.6408 0021074 3.2722 50.4872 14.97664823964449
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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