Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9494
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: 1999-025CC
Object number (NORAD): 29786
Object ID (CCSDS): 29786
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.205 minutes
Inclination: 98.7487 deg
SMA: 7241.163 km
Apoapsis: 919.173 km
Periapsis: 806.883 km
RAAN: 149.6143 deg
Eccentricy: 0.0077536
Argument of periapsis: 206.1175 deg
Mean anomaly: 278.4088 deg
Mean motion: 14.08932816 rev/day
Mean motion (dot): 0.00000436 rev/day2
B* drag term: 0.00026947 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 9:02 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29786U 99025CC 25125.87666845 .00000436 00000-0 26947-3 0 9996
TLE line 2: 2 29786 98.7487 149.6143 0077536 206.1175 278.4088 14.08932816940502
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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