Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9558
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: 99.095 minutes
Inclination: 98.1873 deg
SMA: 7093.498 km
Apoapsis: 826.062 km
Periapsis: 604.664 km
RAAN: 290.2037 deg
Eccentricy: 0.0156057
Argument of periapsis: 324.7385 deg
Mean anomaly: 158.2893 deg
Mean motion: 14.53155438 rev/day
Mean motion (dot): 0.00000683 rev/day2
B* drag term: 0.00015166 1/REarth
Two-line elements (TLE)
Creation date: July 10, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 9, 2025, 7:37 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29836U 99025EE 25190.81790361 .00000683 00000-0 15166-3 0 9994
TLE line 2: 2 29836 98.1873 290.2037 0156057 324.7385 158.2893 14.53155438612908
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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