Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025ANM
Object number (NORAD): 30630
Object ID (CCSDS): 30630
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.293 minutes
Inclination: 99.1648 deg
SMA: 7198.0 km
Apoapsis: 838.752 km
Periapsis: 800.978 km
RAAN: 354.0221 deg
Eccentricy: 0.0026239
Argument of periapsis: 166.3715 deg
Mean anomaly: 319.8887 deg
Mean motion: 14.21624865 rev/day
Mean motion (dot): 0.00001331 rev/day2
B* drag term: 0.00062615 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, 6:13 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30630U 99025ANM 25187.25919274 .00001331 00000-0 62615-3 0 9990
TLE line 2: 2 30630 99.1648 354.0221 0026239 166.3715 319.8887 14.21624865949464
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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