Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.1
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: 1999-025BA
Object number (NORAD): 29760
Object ID (CCSDS): 29760
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.266 minutes
Inclination: 98.7608 deg
SMA: 7244.037 km
Apoapsis: 961.708 km
Periapsis: 770.096 km
RAAN: 132.8346 deg
Eccentricy: 0.0132255
Argument of periapsis: 81.8014 deg
Mean anomaly: 279.8132 deg
Mean motion: 14.08094352 rev/day
Mean motion (dot): 0.00000705 rev/day2
B* drag term: 0.00040473 1/REarth
Two-line elements (TLE)
Creation date: May 4, 2025, 5:21 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 7:12 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29760U 99025BA 25124.30011447 .00000705 00000-0 40473-3 0 9996
TLE line 2: 2 29760 98.7608 132.8346 0132255 81.8014 279.8132 14.08094352939628
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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