Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9500
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025AGN
Object number (NORAD): 30475
Object ID (CCSDS): 30475
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.77 minutes
Inclination: 98.7976 deg
SMA: 7220.618 km
Apoapsis: 875.054 km
Periapsis: 809.912 km
RAAN: 177.3591 deg
Eccentricy: 0.0045108
Argument of periapsis: 178.8089 deg
Mean anomaly: 355.9723 deg
Mean motion: 14.14950342 rev/day
Mean motion (dot): 0.000016 rev/day2
B* drag term: 0.0008418 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 10:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 12, 2025, 8:50 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30475U 99025AGN 25132.86856819 .00001600 00000-0 84180-3 0 9999
TLE line 2: 2 30475 98.7976 177.3591 0045108 178.8089 355.9723 14.14950342939579
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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