Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
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: 1999-025CY
Object number (NORAD): 29806
Object ID (CCSDS): 29806
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.008 minutes
Inclination: 98.7208 deg
SMA: 7231.869 km
Apoapsis: 873.913 km
Periapsis: 833.556 km
RAAN: 207.8735 deg
Eccentricy: 0.0027902
Argument of periapsis: 347.8803 deg
Mean anomaly: 132.1997 deg
Mean motion: 14.11649627 rev/day
Mean motion (dot): 0.00000691 rev/day2
B* drag term: 0.00040208 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:29 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29806U 99025CY 25187.64547635 .00000691 00000-0 40208-3 0 9996
TLE line 2: 2 29806 98.7208 207.8735 0027902 347.8803 132.1997 14.11649627949067
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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