Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9661
Days in orbit
Revolutions
≈ 14.5
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: 1999-025EE
Object number (NORAD): 29836
Object ID (CCSDS): 29836
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.056 minutes
Inclination: 98.189 deg
SMA: 7091.629 km
Apoapsis: 823.823 km
Periapsis: 603.164 km
RAAN: 30.3273 deg
Eccentricy: 0.01555773
Argument of periapsis: 8.5176 deg
Mean anomaly: 19.8648 deg
Mean motion: 14.53730049 rev/day
Mean motion (dot): 0.00003338 rev/day2
B* drag term: 0.00068866847 1/REarth
Two-line elements (TLE)
Creation date: Oct. 20, 2025, 10:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 20, 2025, 5:47 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29836U 99025EE 25293.24135449 .00003338 00000-0 68867-3 0 9991
TLE line 2: 2 29836 98.1890 30.3273 0155577 8.5176 19.8648 14.53730049627782
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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