Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.3
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: 1999-025AMB
Object number (NORAD): 30596
Object ID (CCSDS): 30596
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.438 minutes
Inclination: 98.4066 deg
SMA: 7157.439 km
Apoapsis: 957.984 km
Periapsis: 600.625 km
RAAN: 130.9859 deg
Eccentricy: 0.0249641
Argument of periapsis: 221.2296 deg
Mean anomaly: 266.9361 deg
Mean motion: 14.3372624 rev/day
Mean motion (dot): 0.00000794 rev/day2
B* drag term: 0.00021524 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, 12:43 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30596U 99025AMB 25127.53035926 .00000794 00000-0 21524-3 0 9995
TLE line 2: 2 30596 98.4066 130.9859 0249641 221.2296 266.9361 14.33726240954196
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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