Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
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: 1999-025AVQ
Object number (NORAD): 30830
Object ID (CCSDS): 30830
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.981 minutes
Inclination: 98.7145 deg
SMA: 7230.582 km
Apoapsis: 873.931 km
Periapsis: 830.963 km
RAAN: 180.1418 deg
Eccentricy: 0.0029713
Argument of periapsis: 284.0276 deg
Mean anomaly: 233.1098 deg
Mean motion: 14.12026596 rev/day
Mean motion (dot): 0.00000299 rev/day2
B* drag term: 0.00018585 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, 10:55 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30830U 99025AVQ 25187.45527199 .00000299 00000-0 18585-3 0 9994
TLE line 2: 2 30830 98.7145 180.1418 0029713 284.0276 233.1098 14.12026596943518
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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