Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9494
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: 101.932 minutes
Inclination: 98.607 deg
SMA: 7228.279 km
Apoapsis: 922.781 km
Periapsis: 777.507 km
RAAN: 139.9805 deg
Eccentricy: 0.010049
Argument of periapsis: 71.8772 deg
Mean anomaly: 289.3314 deg
Mean motion: 14.1270151 rev/day
Mean motion (dot): 0.00002044 rev/day2
B* drag term: 0.0010715 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 2, 2025, 7:02 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38510U 99025ESV 25122.29343340 .00002044 00000-0 10715-2 0 9998
TLE line 2: 2 38510 98.6070 139.9805 0100490 71.8772 289.3314 14.12701510855000
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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