Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 14.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.9
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: 1999-025CEL
Object number (NORAD): 31737
Object ID (CCSDS): 31737
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.166 minutes
Inclination: 97.9383 deg
SMA: 7049.115 km
Apoapsis: 778.527 km
Periapsis: 563.433 km
RAAN: 167.6758 deg
Eccentricy: 0.0152568
Argument of periapsis: 353.7659 deg
Mean anomaly: 63.6994 deg
Mean motion: 14.66901268 rev/day
Mean motion (dot): 0.00004267 rev/day2
B* drag term: 0.0006491 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 8:04 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31737U 99025CEL 25127.33648238 .00004267 00000-0 64910-3 0 9992
TLE line 2: 2 31737 97.9383 167.6758 0152568 353.7659 63.6994 14.66901268949818
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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