Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9619
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: 100.545 minutes
Inclination: 98.8807 deg
SMA: 7162.556 km
Apoapsis: 799.032 km
Periapsis: 769.811 km
RAAN: 340.4987 deg
Eccentricy: 0.00203989
Argument of periapsis: 338.6228 deg
Mean anomaly: 21.4101 deg
Mean motion: 14.32190164 rev/day
Mean motion (dot): 0.00004654 rev/day2
B* drag term: 0.0017401706 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 9:49 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 11:30 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 35165U 99025DMV 25250.97937160 .00004654 00000-0 17402-2 0 9996
TLE line 2: 2 35165 98.8807 340.4987 0020399 338.6228 21.4101 14.32190164883494
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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