Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9494
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.7
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: 1999-025EGW
Object number (NORAD): 37428
Object ID (CCSDS): 37428
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.555 minutes
Inclination: 97.7447 deg
SMA: 7162.993 km
Apoapsis: 828.059 km
Periapsis: 741.658 km
RAAN: 5.7757 deg
Eccentricy: 0.0060311
Argument of periapsis: 68.5602 deg
Mean anomaly: 292.2002 deg
Mean motion: 14.32059092 rev/day
Mean motion (dot): 0.00008512 rev/day2
B* drag term: 0.0031157 1/REarth
Two-line elements (TLE)
Creation date: April 29, 2025, 6:36 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 28, 2025, 10:26 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37428U 99025EGW 25118.93520864 .00008512 00000-0 31157-2 0 9998
TLE line 2: 2 37428 97.7447 5.7757 0060311 68.5602 292.2002 14.32059092913974
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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