Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9617
Days in orbit
Revolutions
≈ 14.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.6
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: 1999-025ESY
Object number (NORAD): 38513
Object ID (CCSDS): 38513
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.835 minutes
Inclination: 97.631 deg
SMA: 7033.232 km
Apoapsis: 839.819 km
Periapsis: 470.375 km
RAAN: 152.6635 deg
Eccentricy: 0.02626414
Argument of periapsis: 213.559 deg
Mean anomaly: 144.8743 deg
Mean motion: 14.71873 rev/day
Mean motion (dot): 0.00019753 rev/day2
B* drag term: 0.0018273014 1/REarth
Two-line elements (TLE)
Creation date: Sept. 2, 2025, 11:42 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 11:17 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38513U 99025ESY 25245.47041923 .00019753 00000-0 18273-2 0 9991
TLE line 2: 2 38513 97.6310 152.6635 0262641 213.5590 144.8743 14.71873000621665
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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