Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9660
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.2
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: 1999-025BH
Object number (NORAD): 29767
Object ID (CCSDS): 29767
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.651 minutes
Inclination: 98.1924 deg
SMA: 7262.216 km
Apoapsis: 1124.682 km
Periapsis: 643.481 km
RAAN: 265.9405 deg
Eccentricy: 0.03313043
Argument of periapsis: 217.3455 deg
Mean anomaly: 200.32 deg
Mean motion: 14.0281042 rev/day
Mean motion (dot): 0.00005118 rev/day2
B* drag term: 0.0020512329 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 9:58 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29767U 99025BH 25291.91560993 .00005118 00000-0 20512-2 0 9994
TLE line 2: 2 29767 98.1924 265.9405 0331304 217.3455 200.3200 14.02810420948312
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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