Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.2
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: 1999-025ELC
Object number (NORAD): 37687
Object ID (CCSDS): 37687
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.116 minutes
Inclination: 98.2033 deg
SMA: 7331.138 km
Apoapsis: 1205.513 km
Periapsis: 700.494 km
RAAN: 234.4853 deg
Eccentricy: 0.0344434
Argument of periapsis: 103.8891 deg
Mean anomaly: 325.2477 deg
Mean motion: 13.83074736 rev/day
Mean motion (dot): 0.00003303 rev/day2
B* drag term: 0.0019305 1/REarth
Two-line elements (TLE)
Creation date: June 27, 2025, 5:57 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 27, 2025, 10:08 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37687U 99025ELC 25178.42245553 .00003303 00000-0 19305-2 0 9998
TLE line 2: 2 37687 98.2033 234.4853 0344434 103.8891 325.2477 13.83074736809266
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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