Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 97.426 minutes
Inclination: 99.1521 deg
SMA: 7013.616 km
Apoapsis: 664.268 km
Periapsis: 606.694 km
RAAN: 115.2643 deg
Eccentricy: 0.0041045
Argument of periapsis: 119.3374 deg
Mean anomaly: 241.1943 deg
Mean motion: 14.78052252 rev/day
Mean motion (dot): 0.00036486 rev/day2
B* drag term: 0.0049638 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 2:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 4:51 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38726U 99025ETT 25124.70270054 .00036486 00000-0 49638-2 0 9999
TLE line 2: 2 38726 99.1521 115.2643 0041045 119.3374 241.1943 14.78052252733507
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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