Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9498
Days in orbit
Revolutions
≈ 14.5
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: 1999-025YA
Object number (NORAD): 30265
Object ID (CCSDS): 30265
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.067 minutes
Inclination: 98.6591 deg
SMA: 7092.186 km
Apoapsis: 734.977 km
Periapsis: 693.125 km
RAAN: 231.3356 deg
Eccentricy: 0.0029506
Argument of periapsis: 313.7794 deg
Mean anomaly: 75.7693 deg
Mean motion: 14.53558696 rev/day
Mean motion (dot): 0.00011137 rev/day2
B* drag term: 0.0026597 1/REarth
Two-line elements (TLE)
Creation date: May 10, 2025, 5:27 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 10, 2025, 5:39 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30265U 99025YA 25130.23560755 .00011137 00000-0 26597-2 0 9999
TLE line 2: 2 30265 98.6591 231.3356 0029506 313.7794 75.7693 14.53558696952527
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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