Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.3
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: 1999-025AGT
Object number (NORAD): 30481
Object ID (CCSDS): 30481
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.137 minutes
Inclination: 98.3491 deg
SMA: 7143.162 km
Apoapsis: 926.957 km
Periapsis: 603.097 km
RAAN: 150.8022 deg
Eccentricy: 0.0226692
Argument of periapsis: 197.747 deg
Mean anomaly: 292.1917 deg
Mean motion: 14.38026855 rev/day
Mean motion (dot): 0.00001623 rev/day2
B* drag term: 0.00041062 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, 2:41 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30481U 99025AGT 25127.61236090 .00001623 00000-0 41062-3 0 9993
TLE line 2: 2 30481 98.3491 150.8022 0226692 197.7470 292.1917 14.38026855953338
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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