Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9616
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025EMD
Object number (NORAD): 37712
Object ID (CCSDS): 37712
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.28 minutes
Inclination: 98.8075 deg
SMA: 7149.94 km
Apoapsis: 828.32 km
Periapsis: 715.29 km
RAAN: 24.9173 deg
Eccentricy: 0.00790423
Argument of periapsis: 283.839 deg
Mean anomaly: 254.6904 deg
Mean motion: 14.35982531 rev/day
Mean motion (dot): 0.00001974 rev/day2
B* drag term: 0.00067152039 1/REarth
Two-line elements (TLE)
Creation date: Sept. 5, 2025, 10:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 3:40 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37712U 99025EMD 25248.15319332 .00001974 00000-0 67152-3 0 9998
TLE line 2: 2 37712 98.8075 24.9173 0079042 283.8390 254.6904 14.35982531625453
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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