Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 14.2
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: 1999-025BTR
Object number (NORAD): 31429
Object ID (CCSDS): 31429
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.281 minutes
Inclination: 98.7055 deg
SMA: 7197.455 km
Apoapsis: 830.66 km
Periapsis: 807.98 km
RAAN: 237.7322 deg
Eccentricy: 0.0015756
Argument of periapsis: 156.258 deg
Mean anomaly: 355.869 deg
Mean motion: 14.2178628 rev/day
Mean motion (dot): 0.00001415 rev/day2
B* drag term: 0.00066192 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 10:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 2:56 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31429U 99025BTR 25186.62254931 .00001415 00000-0 66192-3 0 9996
TLE line 2: 2 31429 98.7055 237.7322 0015756 156.2580 355.8690 14.21786280937523
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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