Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.5
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: 1999-025EAW
Object number (NORAD): 36724
Object ID (CCSDS): 36724
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.035 minutes
Inclination: 99.4684 deg
SMA: 7185.811 km
Apoapsis: 882.176 km
Periapsis: 733.176 km
RAAN: 15.5672 deg
Eccentricy: 0.01036768
Argument of periapsis: 205.2556 deg
Mean anomaly: 186.4891 deg
Mean motion: 14.25243591 rev/day
Mean motion (dot): 0.00006383 rev/day2
B* drag term: 0.0025842278 1/REarth
Two-line elements (TLE)
Creation date: Dec. 10, 2025, 10:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 10, 2025, 1:02 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 36724U 99025EAW 25344.04370294 .00006383 00000-0 25842-2 0 9997
TLE line 2: 2 36724 99.4684 15.5672 0103677 205.2556 186.4891 14.25243591574345
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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