Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9613
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025EQB
Object number (NORAD): 38130
Object ID (CCSDS): 38130
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.588 minutes
Inclination: 98.609 deg
SMA: 7353.303 km
Apoapsis: 1129.898 km
Periapsis: 820.438 km
RAAN: 305.7176 deg
Eccentricy: 0.02104229
Argument of periapsis: 141.0956 deg
Mean anomaly: 220.5555 deg
Mean motion: 13.76826059 rev/day
Mean motion (dot): 0.00003268 rev/day2
B* drag term: 0.002851961 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 7:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 1, 2025, 9:31 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38130U 99025EQB 25244.39708244 .00003268 00000-0 28520-2 0 9992
TLE line 2: 2 38130 98.6090 305.7176 0210423 141.0956 220.5555 13.76826059678749
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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