Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025DCL
Object number (NORAD): 33603
Object ID (CCSDS): 33603
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.303 minutes
Inclination: 98.8043 deg
SMA: 7007.742 km
Apoapsis: 784.208 km
Periapsis: 475.006 km
RAAN: 281.1129 deg
Eccentricy: 0.02206149
Argument of periapsis: 76.3404 deg
Mean anomaly: 286.2265 deg
Mean motion: 14.79910953 rev/day
Mean motion (dot): 0.00003584 rev/day2
B* drag term: 0.00031974719 1/REarth
Two-line elements (TLE)
Creation date: Dec. 11, 2025, 7:14 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 12:57 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 33603U 99025DCL 25345.54020842 .00003584 00000-0 31975-3 0 9992
TLE line 2: 2 33603 98.8043 281.1129 0220615 76.3404 286.2265 14.79910953988423
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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