Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
100.5
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: 1999-025TJ
Object number (NORAD): 30153
Object ID (CCSDS): 30153
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.441 minutes
Inclination: 100.4668 deg
SMA: 7346.375 km
Apoapsis: 1115.683 km
Periapsis: 820.797 km
RAAN: 337.9627 deg
Eccentricy: 0.02007016
Argument of periapsis: 3.69 deg
Mean anomaly: 114.8244 deg
Mean motion: 13.78774107 rev/day
Mean motion (dot): 0.00002182 rev/day2
B* drag term: 0.0018906535 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, noon UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30153U 99025TJ 25347.50027844 .00002182 00000-0 18907-2 0 9998
TLE line 2: 2 30153 100.4668 337.9627 0200702 3.6900 114.8244 13.78774107947857
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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