Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.3
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: 1999-025DMV
Object number (NORAD): 35165
Object ID (CCSDS): 35165
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.586 minutes
Inclination: 98.8806 deg
SMA: 7164.479 km
Apoapsis: 803.24 km
Periapsis: 769.448 km
RAAN: 267.6511 deg
Eccentricy: 0.0023583
Argument of periapsis: 181.7703 deg
Mean anomaly: 178.34 deg
Mean motion: 14.3161367 rev/day
Mean motion (dot): 0.00002772 rev/day2
B* drag term: 0.001055 1/REarth
Two-line elements (TLE)
Creation date: July 1, 2025, 2:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 28, 2025, 6:33 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 35165U 99025DMV 25179.77319843 .00002772 00000-0 10550-2 0 9992
TLE line 2: 2 35165 98.8806 267.6511 0023583 181.7703 178.3400 14.31613670873303
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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