Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9664
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: 102.06 minutes
Inclination: 99.2262 deg
SMA: 7234.315 km
Apoapsis: 920.488 km
Periapsis: 791.872 km
RAAN: 262.5521 deg
Eccentricy: 0.00888931
Argument of periapsis: 204.1395 deg
Mean anomaly: 155.5597 deg
Mean motion: 14.10933705 rev/day
Mean motion (dot): 0.00004998 rev/day2
B* drag term: 0.0027072621 1/REarth
Two-line elements (TLE)
Creation date: Oct. 23, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 22, 2025, 8:20 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37912U 99025ENM 25295.34779692 .00004998 00000-0 27073-2 0 9998
TLE line 2: 2 37912 99.2262 262.5521 0088893 204.1395 155.5597 14.10933705765634
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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