Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9678
Days in orbit
Revolutions
≈ 13.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.5
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: 1999-025EUM
Object number (NORAD): 38797
Object ID (CCSDS): 38797
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.761 minutes
Inclination: 99.4838 deg
SMA: 7408.146 km
Apoapsis: 1212.488 km
Periapsis: 847.533 km
RAAN: 200.3893 deg
Eccentricy: 0.02463198
Argument of periapsis: 324.4564 deg
Mean anomaly: 34.0382 deg
Mean motion: 13.61565319 rev/day
Mean motion (dot): 0.00000555 rev/day2
B* drag term: 0.00063994347 1/REarth
Two-line elements (TLE)
Creation date: Nov. 4, 2025, 4:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Nov. 2, 2025, 10:19 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38797U 99025EUM 25306.43026401 .00000555 00000-0 63994-3 0 9994
TLE line 2: 2 38797 99.4838 200.3893 0246320 324.4564 34.0382 13.61565319587344
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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