Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9617
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025ENM
Object number (NORAD): 37912
Object ID (CCSDS): 37912
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.105 minutes
Inclination: 99.222 deg
SMA: 7236.424 km
Apoapsis: 926.65 km
Periapsis: 789.928 km
RAAN: 209.7055 deg
Eccentricy: 0.00944685
Argument of periapsis: 349.6867 deg
Mean anomaly: 10.2363 deg
Mean motion: 14.10317042 rev/day
Mean motion (dot): 0.00008948 rev/day2
B* drag term: 0.0048577712 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 31, 2025, 8:28 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37912U 99025ENM 25243.85313760 .00008948 00000-0 48578-2 0 9999
TLE line 2: 2 37912 99.2220 209.7055 0094469 349.6867 10.2363 14.10317042758379
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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