Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9562
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
102.3
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: 1999-025CAJ
Object number (NORAD): 31628
Object ID (CCSDS): 31628
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.906 minutes
Inclination: 102.2739 deg
SMA: 7321.275 km
Apoapsis: 1067.825 km
Periapsis: 818.455 km
RAAN: 2.0981 deg
Eccentricy: 0.0170305
Argument of periapsis: 222.008 deg
Mean anomaly: 136.7899 deg
Mean motion: 13.8587073 rev/day
Mean motion (dot): 0.000019 rev/day2
B* drag term: 0.0015313 1/REarth
Two-line elements (TLE)
Creation date: July 13, 2025, 6:56 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 13, 2025, 5:01 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31628U 99025CAJ 25194.20910066 .00001900 00000-0 15313-2 0 9995
TLE line 2: 2 31628 102.2739 2.0981 0170305 222.0080 136.7899 13.85870730913970
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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