Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9498
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025DFK
Object number (NORAD): 33674
Object ID (CCSDS): 33674
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.649 minutes
Inclination: 98.6118 deg
SMA: 7356.161 km
Apoapsis: 1135.975 km
Periapsis: 820.077 km
RAAN: 200.4998 deg
Eccentricy: 0.0214717
Argument of periapsis: 103.904 deg
Mean anomaly: 258.6096 deg
Mean motion: 13.76023744 rev/day
Mean motion (dot): 0.00002041 rev/day2
B* drag term: 0.0018069 1/REarth
Two-line elements (TLE)
Creation date: May 10, 2025, 5:27 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 10, 2025, 3:20 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 33674U 99025DFK 25130.13930645 .00002041 00000-0 18069-2 0 9993
TLE line 2: 2 33674 98.6118 200.4998 0214717 103.9040 258.6096 13.76023744853851
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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