Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9498
Days in orbit
Revolutions
≈ 11.9
Per day
Orbit
MEO
Medium Earth Orbit
Inclination
99.0
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: 1999-025EJW
Object number (NORAD): 37476
Object ID (CCSDS): 37476
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 120.976 minutes
Inclination: 98.9546 deg
SMA: 8102.616 km
Apoapsis: 2595.044 km
Periapsis: 853.919 km
RAAN: 212.4323 deg
Eccentricy: 0.1074421
Argument of periapsis: 312.6191 deg
Mean anomaly: 38.8963 deg
Mean motion: 11.90323031 rev/day
Mean motion (dot): 0.0000261 rev/day2
B* drag term: 0.0070357 1/REarth
Two-line elements (TLE)
Creation date: April 27, 2025, 2:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 26, 2025, 12:12 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37476U 99025EJW 25116.50853629 .00002610 00000-0 70357-2 0 9998
TLE line 2: 2 37476 98.9546 212.4323 1074421 312.6191 38.8963 11.90323031647039
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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