Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025AEY
Object number (NORAD): 30437
Object ID (CCSDS): 30437
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.274 minutes
Inclination: 98.927 deg
SMA: 7006.361 km
Apoapsis: 655.569 km
Periapsis: 600.882 km
RAAN: 190.2377 deg
Eccentricy: 0.0039027
Argument of periapsis: 241.2294 deg
Mean anomaly: 147.3833 deg
Mean motion: 14.80348721 rev/day
Mean motion (dot): 0.00009389 rev/day2
B* drag term: 0.0012222 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 11:18 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30437U 99025AEY 25188.97105131 .00009389 00000-0 12222-2 0 9993
TLE line 2: 2 30437 98.9270 190.2377 0039027 241.2294 147.3833 14.80348721968480
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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