Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025CMK
Object number (NORAD): 31934
Object ID (CCSDS): 31934
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 96.411 minutes
Inclination: 98.8981 deg
SMA: 6964.858 km
Apoapsis: 619.316 km
Periapsis: 554.131 km
RAAN: 214.6409 deg
Eccentricy: 0.0046796
Argument of periapsis: 30.6816 deg
Mean anomaly: 329.7122 deg
Mean motion: 14.9360008 rev/day
Mean motion (dot): 0.00021855 rev/day2
B* drag term: 0.0020283 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, 12:56 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31934U 99025CMK 25187.53943753 .00021855 00000-0 20283-2 0 9995
TLE line 2: 2 31934 98.8981 214.6409 0046796 30.6816 329.7122 14.93600080584584
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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