Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9615
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025AWV
Object number (NORAD): 30859
Object ID (CCSDS): 30859
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.579 minutes
Inclination: 98.925 deg
SMA: 7116.582 km
Apoapsis: 760.295 km
Periapsis: 716.598 km
RAAN: 291.8155 deg
Eccentricy: 0.00307007
Argument of periapsis: 327.5532 deg
Mean anomaly: 32.377 deg
Mean motion: 14.46090907 rev/day
Mean motion (dot): 0.00012917 rev/day2
B* drag term: 0.0036053105 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 2:22 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30859U 99025AWV 25247.09900174 .00012917 00000-0 36053-2 0 9999
TLE line 2: 2 30859 98.9250 291.8155 0030701 327.5532 32.3770 14.46090907955932
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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