Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9617
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025AEG
Object number (NORAD): 30417
Object ID (CCSDS): 30417
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.802 minutes
Inclination: 98.6862 deg
SMA: 7222.134 km
Apoapsis: 890.8 km
Periapsis: 797.197 km
RAAN: 242.4863 deg
Eccentricy: 0.00648027
Argument of periapsis: 37.9548 deg
Mean anomaly: 21.7026 deg
Mean motion: 14.1450498 rev/day
Mean motion (dot): 0.00000884 rev/day2
B* drag term: 0.00047364435 1/REarth
Two-line elements (TLE)
Creation date: Sept. 7, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 10:20 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30417U 99025AEG 25249.93063718 .00000884 00000-0 47364-3 0 9996
TLE line 2: 2 30417 98.6862 242.4863 0064803 37.9548 21.7026 14.14504980960203
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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