Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.3
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: 1999-025EZM
Object number (NORAD): 46987
Object ID (CCSDS): 46987
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.584 minutes
Inclination: 98.8958 deg
SMA: 7164.412 km
Apoapsis: 816.965 km
Periapsis: 755.59 km
RAAN: 27.685 deg
Eccentricy: 0.0042833
Argument of periapsis: 187.0295 deg
Mean anomaly: 173.0292 deg
Mean motion: 14.31633622 rev/day
Mean motion (dot): 0.00042095 rev/day2
B* drag term: 0.015565 1/REarth
Two-line elements (TLE)
Creation date: May 21, 2025, 4:08 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 5, 2024, 6:12 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 46987U 99025EZM 24279.25900186 .00042095 00000-0 15565-1 0 9997
TLE line 2: 2 46987 98.8958 27.6850 0042833 187.0295 173.0292 14.31633622511083
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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