Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
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: 1999-025EWJ
Object number (NORAD): 39541
Object ID (CCSDS): 39541
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.432 minutes
Inclination: 98.7016 deg
SMA: 7204.6 km
Apoapsis: 878.851 km
Periapsis: 774.079 km
RAAN: 152.2053 deg
Eccentricy: 0.0072712
Argument of periapsis: 48.0284 deg
Mean anomaly: 312.7057 deg
Mean motion: 14.19671677 rev/day
Mean motion (dot): 0.00002405 rev/day2
B* drag term: 0.0011277 1/REarth
Two-line elements (TLE)
Creation date: April 15, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 15, 2025, 8:49 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 39541U 99025EWJ 25105.86802541 .00002405 00000-0 11277-2 0 9995
TLE line 2: 2 39541 98.7016 152.2053 0072712 48.0284 312.7057 14.19671677581499
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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