Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9664
Days in orbit
Revolutions
≈ 14.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025DMH
Object number (NORAD): 35153
Object ID (CCSDS): 35153
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.739 minutes
Inclination: 98.9041 deg
SMA: 7028.656 km
Apoapsis: 770.003 km
Periapsis: 531.039 km
RAAN: 181.6679 deg
Eccentricy: 0.0169993
Argument of periapsis: 245.0448 deg
Mean anomaly: 113.3014 deg
Mean motion: 14.73310576 rev/day
Mean motion (dot): 0.00005003 rev/day2
B* drag term: 0.00062285 1/REarth
Two-line elements (TLE)
Creation date: Oct. 22, 2025, 6:36 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 9:46 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 35153U 99025DMH 25294.90762213 .00005003 00000-0 62285-3 0 9998
TLE line 2: 2 35153 98.9041 181.6679 0169993 245.0448 113.3014 14.73310576964540
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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