Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9491
Days in orbit
Revolutions
≈ 13.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.4
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: 1999-025CMA
Object number (NORAD): 31923
Object ID (CCSDS): 31923
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 106.323 minutes
Inclination: 98.4284 deg
SMA: 7434.406 km
Apoapsis: 1282.553 km
Periapsis: 829.988 km
RAAN: 248.0174 deg
Eccentricy: 0.0304372
Argument of periapsis: 170.0819 deg
Mean anomaly: 190.6516 deg
Mean motion: 13.54357657 rev/day
Mean motion (dot): 0.00002977 rev/day2
B* drag term: 0.0032873 1/REarth
Two-line elements (TLE)
Creation date: May 2, 2025, 2:33 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 1, 2025, 7:03 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31923U 99025CMA 25121.79411657 .00002977 00000-0 32873-2 0 9994
TLE line 2: 2 31923 98.4284 248.0174 0304372 170.0819 190.6516 13.54357657605898
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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