Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
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: 103.712 minutes
Inclination: 98.5656 deg
SMA: 7312.153 km
Apoapsis: 1175.227 km
Periapsis: 692.81 km
RAAN: 302.961 deg
Eccentricy: 0.0329873
Argument of periapsis: 67.3262 deg
Mean anomaly: 324.9963 deg
Mean motion: 13.88464639 rev/day
Mean motion (dot): 0.00003428 rev/day2
B* drag term: 0.0018686 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 10:16 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31426U 99025BTN 25128.42824755 .00003428 00000-0 18686-2 0 9994
TLE line 2: 2 31426 98.5656 302.9610 0329873 67.3262 324.9963 13.88464639905424
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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