Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9553
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025AFJ
Object number (NORAD): 30447
Object ID (CCSDS): 30447
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.112 minutes
Inclination: 98.9873 deg
SMA: 7094.31 km
Apoapsis: 760.254 km
Periapsis: 672.096 km
RAAN: 35.3916 deg
Eccentricy: 0.0062133
Argument of periapsis: 157.7757 deg
Mean anomaly: 228.986 deg
Mean motion: 14.52905883 rev/day
Mean motion (dot): 0.00007353 rev/day2
B* drag term: 0.0017519 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 1:34 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30447U 99025AFJ 25185.56577019 .00007353 00000-0 17519-2 0 9997
TLE line 2: 2 30447 98.9873 35.3916 0062133 157.7757 228.9860 14.52905883957534
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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