Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.1
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: 1999-025ETT
Object number (NORAD): 38726
Object ID (CCSDS): 38726
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.172 minutes
Inclination: 99.1487 deg
SMA: 7001.466 km
Apoapsis: 644.977 km
Periapsis: 601.684 km
RAAN: 184.7777 deg
Eccentricy: 0.0030917
Argument of periapsis: 292.7216 deg
Mean anomaly: 67.0726 deg
Mean motion: 14.81901402 rev/day
Mean motion (dot): 0.00024021 rev/day2
B* drag term: 0.0030085 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 4:36 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 5:54 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38726U 99025ETT 25185.74623743 .00024021 00000-0 30085-2 0 9995
TLE line 2: 2 38726 99.1487 184.7777 0030917 292.7216 67.0726 14.81901402674584
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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