Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.3
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: 1999-025EVD
Object number (NORAD): 38813
Object ID (CCSDS): 38813
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.437 minutes
Inclination: 99.3345 deg
SMA: 7204.839 km
Apoapsis: 831.735 km
Periapsis: 821.672 km
RAAN: 109.1961 deg
Eccentricy: 0.0006983
Argument of periapsis: 35.2963 deg
Mean anomaly: 324.8672 deg
Mean motion: 14.19601284 rev/day
Mean motion (dot): 0.00001655 rev/day2
B* drag term: 0.00080693 1/REarth
Two-line elements (TLE)
Creation date: May 4, 2025, 5:21 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 4:31 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38813U 99025EVD 25124.18844080 .00001655 00000-0 80693-3 0 9991
TLE line 2: 2 38813 99.3345 109.1961 0006983 35.2963 324.8672 14.19601284450927
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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