Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.2
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: 1999-025EYE
Object number (NORAD): 41827
Object ID (CCSDS): 41827
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.152 minutes
Inclination: 98.7506 deg
SMA: 7191.321 km
Apoapsis: 855.965 km
Periapsis: 770.407 km
RAAN: 197.2904 deg
Eccentricy: 0.0059487
Argument of periapsis: 130.9689 deg
Mean anomaly: 229.6658 deg
Mean motion: 14.23605903 rev/day
Mean motion (dot): 0.00004286 rev/day2
B* drag term: 0.0018649 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, 3:46 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 41827U 99025EYE 25127.15746518 .00004286 00000-0 18649-2 0 9991
TLE line 2: 2 41827 98.7506 197.2904 0059487 130.9689 229.6658 14.23605903442056
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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