Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025CU
Object number (NORAD): 29802
Object ID (CCSDS): 29802
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.83 minutes
Inclination: 98.6169 deg
SMA: 7080.866 km
Apoapsis: 733.447 km
Periapsis: 672.015 km
RAAN: 289.248 deg
Eccentricy: 0.0043379
Argument of periapsis: 114.8546 deg
Mean anomaly: 309.1795 deg
Mean motion: 14.57045708 rev/day
Mean motion (dot): 0.00009863 rev/day2
B* drag term: 0.0021722 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 5:07 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29802U 99025CU 25186.21380690 .00009863 00000-0 21722-2 0 9999
TLE line 2: 2 29802 98.6169 289.2480 0043379 114.8546 309.1795 14.57045708961326
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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