Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
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: 104.636 minutes
Inclination: 98.6133 deg
SMA: 7355.526 km
Apoapsis: 1130.178 km
Periapsis: 824.604 km
RAAN: 252.1174 deg
Eccentricy: 0.0207717
Argument of periapsis: 310.1009 deg
Mean anomaly: 48.2097 deg
Mean motion: 13.76201967 rev/day
Mean motion (dot): 0.00001425 rev/day2
B* drag term: 0.0012837 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:23 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 33674U 99025DFK 25187.14120082 .00001425 00000-0 12837-2 0 9994
TLE line 2: 2 33674 98.6133 252.1174 0207717 310.1009 48.2097 13.76201967861697
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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