Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9553
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025BTN
Object number (NORAD): 31426
Object ID (CCSDS): 31426
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.695 minutes
Inclination: 98.5681 deg
SMA: 7311.362 km
Apoapsis: 1171.961 km
Periapsis: 694.493 km
RAAN: 355.4455 deg
Eccentricy: 0.0326525
Argument of periapsis: 270.1832 deg
Mean anomaly: 116.0215 deg
Mean motion: 13.88690067 rev/day
Mean motion (dot): 0.00001902 rev/day2
B* drag term: 0.0010536 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 10:08 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31426U 99025BTN 25185.42275942 .00001902 00000-0 10536-2 0 9996
TLE line 2: 2 31426 98.5681 355.4455 0326525 270.1832 116.0215 13.88690067913335
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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