Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9619
Days in orbit
Revolutions
≈ 14.2
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: 1999-025EYL
Object number (NORAD): 41833
Object ID (CCSDS): 41833
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.068 minutes
Inclination: 98.7548 deg
SMA: 7187.359 km
Apoapsis: 849.61 km
Periapsis: 768.837 km
RAAN: 320.7279 deg
Eccentricy: 0.00561905
Argument of periapsis: 142.7734 deg
Mean anomaly: 217.7361 deg
Mean motion: 14.24783244 rev/day
Mean motion (dot): 0.0000413 rev/day2
B* drag term: 0.0017607397 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 3:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 10:02 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 41833U 99025EYL 25250.91816916 .00004130 00000-0 17607-2 0 9990
TLE line 2: 2 41833 98.7548 320.7279 0056191 142.7734 217.7361 14.24783244459994
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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