Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9714
Days in orbit
Revolutions
≈ 14.3
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: 1999-025CE
Object number (NORAD): 29788
Object ID (CCSDS): 29788
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 100.984 minutes
Inclination: 98.7839 deg
SMA: 7183.383 km
Apoapsis: 836.202 km
Periapsis: 774.295 km
RAAN: 57.7855 deg
Eccentricy: 0.00430906
Argument of periapsis: 190.57 deg
Mean anomaly: 232.2312 deg
Mean motion: 14.25966117 rev/day
Mean motion (dot): 0.00006186 rev/day2
B* drag term: 0.0025856412 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 3:55 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29788U 99025CE 25346.16342485 .00006186 00000-0 25856-2 0 9991
TLE line 2: 2 29788 98.7839 57.7855 0043091 190.5700 232.2312 14.25966117973473
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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