Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9492
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: 1999-025EAD
Object number (NORAD): 36707
Object ID (CCSDS): 36707
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.66 minutes
Inclination: 98.77 deg
SMA: 7215.38 km
Apoapsis: 873.491 km
Periapsis: 800.999 km
RAAN: 167.8834 deg
Eccentricy: 0.0050234
Argument of periapsis: 56.8745 deg
Mean anomaly: 303.7236 deg
Mean motion: 14.16491369 rev/day
Mean motion (dot): 0.00002842 rev/day2
B* drag term: 0.0014315 1/REarth
Two-line elements (TLE)
Creation date: April 29, 2025, 4:35 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 28, 2025, 9:44 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 36707U 99025EAD 25118.40606382 .00002842 00000-0 14315-2 0 9996
TLE line 2: 2 36707 98.7700 167.8834 0050234 56.8745 303.7236 14.16491369608464
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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