Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025EHG
Object number (NORAD): 37438
Object ID (CCSDS): 37438
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.767 minutes
Inclination: 98.7535 deg
SMA: 7220.439 km
Apoapsis: 863.695 km
Periapsis: 820.914 km
RAAN: 204.3178 deg
Eccentricy: 0.0029625
Argument of periapsis: 34.0008 deg
Mean anomaly: 326.3057 deg
Mean motion: 14.15002963 rev/day
Mean motion (dot): 0.00000827 rev/day2
B* drag term: 0.00044791 1/REarth
Two-line elements (TLE)
Creation date: June 19, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 10, 2025, 8:16 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37438U 99025EHG 25161.84473552 .00000827 00000-0 44791-3 0 9998
TLE line 2: 2 37438 98.7535 204.3178 0029625 34.0008 326.3057 14.15002963882496
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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