Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025BF
Object number (NORAD): 29765
Object ID (CCSDS): 29765
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.703 minutes
Inclination: 98.841 deg
SMA: 7264.651 km
Apoapsis: 929.428 km
Periapsis: 843.604 km
RAAN: 210.6914 deg
Eccentricy: 0.005907
Argument of periapsis: 174.5228 deg
Mean anomaly: 305.698 deg
Mean motion: 14.02105317 rev/day
Mean motion (dot): 0.00000079 rev/day2
B* drag term: 0.000078404 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:26 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29765U 99025BF 25187.64373331 .00000079 00000-0 78404-4 0 9990
TLE line 2: 2 29765 98.8410 210.6914 0059070 174.5228 305.6980 14.02105317945210
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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