Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.5
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: 1999-025CXH
Object number (NORAD): 32316
Object ID (CCSDS): 32316
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.347 minutes
Inclination: 99.5365 deg
SMA: 7105.555 km
Apoapsis: 746.899 km
Periapsis: 707.941 km
RAAN: 124.4891 deg
Eccentricy: 0.0027414
Argument of periapsis: 259.7124 deg
Mean anomaly: 126.6094 deg
Mean motion: 14.49458404 rev/day
Mean motion (dot): 0.00005423 rev/day2
B* drag term: 0.0014232 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 11:15 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32316U 99025CXH 25126.96935741 .00005423 00000-0 14232-2 0 9998
TLE line 2: 2 32316 99.5365 124.4891 0027414 259.7124 126.6094 14.49458404925918
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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