Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9499
Days in orbit
Revolutions
≈ 14.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025CHJ
Object number (NORAD): 31820
Object ID (CCSDS): 31820
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 96.952 minutes
Inclination: 98.9437 deg
SMA: 6990.881 km
Apoapsis: 729.446 km
Periapsis: 496.047 km
RAAN: 275.0407 deg
Eccentricy: 0.0166931
Argument of periapsis: 337.989 deg
Mean anomaly: 21.4209 deg
Mean motion: 14.85268189 rev/day
Mean motion (dot): 0.00007449 rev/day2
B* drag term: 0.00068167 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 2:31 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 11, 2025, 8:20 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31820U 99025CHJ 25131.84762016 .00007449 00000-0 68167-3 0 9990
TLE line 2: 2 31820 98.9437 275.0407 0166931 337.9890 21.4209 14.85268189950606
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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