Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.0
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: 1999-025MV
Object number (NORAD): 30020
Object ID (CCSDS): 30020
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.555 minutes
Inclination: 98.8445 deg
SMA: 7257.661 km
Apoapsis: 1013.571 km
Periapsis: 745.481 km
RAAN: 196.7633 deg
Eccentricy: 0.0184695
Argument of periapsis: 151.297 deg
Mean anomaly: 229.5795 deg
Mean motion: 14.04131382 rev/day
Mean motion (dot): 0.00000241 rev/day2
B* drag term: 0.00015307 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 11:30 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30020U 99025MV 25188.97961847 .00000241 00000-0 15307-3 0 9991
TLE line 2: 2 30020 98.8445 196.7633 0184695 151.2970 229.5795 14.04131382944449
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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