Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.3
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: 1999-025CAA
Object number (NORAD): 31620
Object ID (CCSDS): 31620
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.418 minutes
Inclination: 98.8915 deg
SMA: 7156.518 km
Apoapsis: 792.363 km
Periapsis: 764.403 km
RAAN: 201.3164 deg
Eccentricy: 0.0019535
Argument of periapsis: 337.8856 deg
Mean anomaly: 22.1483 deg
Mean motion: 14.3400315 rev/day
Mean motion (dot): 0.00007977 rev/day2
B* drag term: 0.0028647 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 10:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 3, 2025, 10:33 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31620U 99025CAA 25123.93967742 .00007977 00000-0 28647-2 0 9996
TLE line 2: 2 31620 98.8915 201.3164 0019535 337.8856 22.1483 14.34003150927328
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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