Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 13.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025ENB
Object number (NORAD): 37902
Object ID (CCSDS): 37902
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 106.514 minutes
Inclination: 98.6923 deg
SMA: 7443.272 km
Apoapsis: 1309.737 km
Periapsis: 820.538 km
RAAN: 56.7448 deg
Eccentricy: 0.0328618
Argument of periapsis: 27.8916 deg
Mean anomaly: 333.9416 deg
Mean motion: 13.51938352 rev/day
Mean motion (dot): 0.0000118 rev/day2
B* drag term: 0.0013209 1/REarth
Two-line elements (TLE)
Creation date: June 29, 2025, 5:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 24, 2025, 2:57 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37902U 99025ENB 25175.62316233 .00001180 00000-0 13209-2 0 9999
TLE line 2: 2 37902 98.6923 56.7448 0328618 27.8916 333.9416 13.51938352606646
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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