Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
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: 1999-025AEH
Object number (NORAD): 30418
Object ID (CCSDS): 30418
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.234 minutes
Inclination: 98.8255 deg
SMA: 7004.441 km
Apoapsis: 707.553 km
Periapsis: 545.06 km
RAAN: 330.6039 deg
Eccentricy: 0.0115993
Argument of periapsis: 261.3705 deg
Mean anomaly: 130.1356 deg
Mean motion: 14.80957154 rev/day
Mean motion (dot): 0.00004435 rev/day2
B* drag term: 0.00051869 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, 8:38 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30418U 99025AEH 25187.36023492 .00004435 00000-0 51869-3 0 9991
TLE line 2: 2 30418 98.8255 330.6039 0115993 261.3705 130.1356 14.80957154982317
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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