Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.6
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: 1999-025EPC
Object number (NORAD): 37927
Object ID (CCSDS): 37927
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.541 minutes
Inclination: 98.8014 deg
SMA: 7067.074 km
Apoapsis: 695.1 km
Periapsis: 682.778 km
RAAN: 251.9703 deg
Eccentricy: 0.0008718
Argument of periapsis: 227.5491 deg
Mean anomaly: 132.4971 deg
Mean motion: 14.61313287 rev/day
Mean motion (dot): 0.00023233 rev/day2
B* drag term: 0.0046969 1/REarth
Two-line elements (TLE)
Creation date: May 4, 2025, 5:21 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 1:59 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37927U 99025EPC 25124.08299342 .00023233 00000-0 46969-2 0 9993
TLE line 2: 2 37927 98.8014 251.9703 0008718 227.5491 132.4971 14.61313287618559
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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