Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
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: 102.025 minutes
Inclination: 99.2302 deg
SMA: 7232.657 km
Apoapsis: 920.481 km
Periapsis: 788.564 km
RAAN: 309.8335 deg
Eccentricy: 0.00911955
Argument of periapsis: 74.9151 deg
Mean anomaly: 286.2087 deg
Mean motion: 14.11418958 rev/day
Mean motion (dot): 0.00007072 rev/day2
B* drag term: 0.0037768803 1/REarth
Two-line elements (TLE)
Creation date: Dec. 8, 2025, 3:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 7, 2025, 8:43 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37912U 99025ENM 25341.36376393 .00007072 00000-0 37769-2 0 9992
TLE line 2: 2 37912 99.2302 309.8335 0091195 74.9151 286.2087 14.11418958772126
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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