Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.1
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: 1999-025ESV
Object number (NORAD): 38510
Object ID (CCSDS): 38510
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.922 minutes
Inclination: 98.6048 deg
SMA: 7227.803 km
Apoapsis: 920.055 km
Periapsis: 779.281 km
RAAN: 199.0893 deg
Eccentricy: 0.0097384
Argument of periapsis: 255.6017 deg
Mean anomaly: 103.4331 deg
Mean motion: 14.1284108 rev/day
Mean motion (dot): 0.00000673 rev/day2
B* drag term: 0.00036805 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 3:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 6:23 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38510U 99025ESV 25183.76657794 .00000673 00000-0 36805-3 0 9993
TLE line 2: 2 38510 98.6048 199.0893 0097384 255.6017 103.4331 14.12841080863685
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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