Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9615
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025EEG
Object number (NORAD): 37048
Object ID (CCSDS): 37048
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.492 minutes
Inclination: 98.9014 deg
SMA: 7395.587 km
Apoapsis: 1205.984 km
Periapsis: 828.92 km
RAAN: 115.9927 deg
Eccentricy: 0.02549248
Argument of periapsis: 52.1441 deg
Mean anomaly: 69.8166 deg
Mean motion: 13.65035009 rev/day
Mean motion (dot): 0.00000931 rev/day2
B* drag term: 0.00095926313 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 4:29 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 10:37 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37048U 99025EEG 25246.44304576 .00000931 00000-0 95926-3 0 9996
TLE line 2: 2 37048 98.9014 115.9927 0254925 52.1441 69.8166 13.65035009608016
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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