Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.4
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: 1999-025DMJ
Object number (NORAD): 35154
Object ID (CCSDS): 35154
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.517 minutes
Inclination: 99.4079 deg
SMA: 7208.638 km
Apoapsis: 960.996 km
Periapsis: 700.01 km
RAAN: 294.959 deg
Eccentricy: 0.0181023
Argument of periapsis: 141.395 deg
Mean anomaly: 220.0329 deg
Mean motion: 14.18478974 rev/day
Mean motion (dot): 0.00000811 rev/day2
B* drag term: 0.00035411 1/REarth
Two-line elements (TLE)
Creation date: July 2, 2025, 5:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 12:38 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 35154U 99025DMJ 25183.52676296 .00000811 00000-0 35411-3 0 9992
TLE line 2: 2 35154 99.4079 294.9590 0181023 141.3950 220.0329 14.18478974622634
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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