Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025EBB
Object number (NORAD): 36729
Object ID (CCSDS): 36729
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.119 minutes
Inclination: 98.6888 deg
SMA: 7237.087 km
Apoapsis: 892.524 km
Periapsis: 825.381 km
RAAN: 173.2406 deg
Eccentricy: 0.0046388
Argument of periapsis: 353.1025 deg
Mean anomaly: 6.9502 deg
Mean motion: 14.10123168 rev/day
Mean motion (dot): 0.00000281 rev/day2
B* drag term: 0.00018114 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, 4:51 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 36729U 99025EBB 25186.20213464 .00000281 00000-0 18114-3 0 9995
TLE line 2: 2 36729 98.6888 173.2406 0046388 353.1025 6.9502 14.10123168849894
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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