Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9664
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.2
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: 1999-025EGS
Object number (NORAD): 37424
Object ID (CCSDS): 37424
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.582 minutes
Inclination: 97.1942 deg
SMA: 7211.698 km
Apoapsis: 990.397 km
Periapsis: 676.729 km
RAAN: 73.3246 deg
Eccentricy: 0.02174714
Argument of periapsis: 77.0637 deg
Mean anomaly: 285.4732 deg
Mean motion: 14.17576357 rev/day
Mean motion (dot): 0.00002867 rev/day2
B* drag term: 0.0011299838 1/REarth
Two-line elements (TLE)
Creation date: Oct. 22, 2025, 5:40 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 22, 2025, 3:01 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37424U 99025EGS 25295.12628363 .00002867 00000-0 11300-2 0 9999
TLE line 2: 2 37424 97.1942 73.3246 0217471 77.0637 285.4732 14.17576357678425
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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