Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.3
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: 1999-025AVM
Object number (NORAD): 30827
Object ID (CCSDS): 30827
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.381 minutes
Inclination: 98.9887 deg
SMA: 7154.77 km
Apoapsis: 808.196 km
Periapsis: 745.075 km
RAAN: 166.4247 deg
Eccentricy: 0.0044111
Argument of periapsis: 286.5501 deg
Mean anomaly: 73.0839 deg
Mean motion: 14.34528606 rev/day
Mean motion (dot): 0.00004524 rev/day2
B* drag term: 0.0016021 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 9:15 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30827U 99025AVM 25187.88580611 .00004524 00000-0 16021-2 0 9992
TLE line 2: 2 30827 98.9887 166.4247 0044111 286.5501 73.0839 14.34528606943509
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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