Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.0
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: 1999-025ADJ
Object number (NORAD): 30395
Object ID (CCSDS): 30395
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.12 minutes
Inclination: 98.9387 deg
SMA: 7284.297 km
Apoapsis: 1024.007 km
Periapsis: 788.317 km
RAAN: 207.6721 deg
Eccentricy: 0.016178
Argument of periapsis: 103.9455 deg
Mean anomaly: 22.935 deg
Mean motion: 13.96436856 rev/day
Mean motion (dot): 0.00000168 rev/day2
B* drag term: 0.00013589 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 2:52 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30395U 99025ADJ 25187.61961544 .00000168 00000-0 13589-3 0 9998
TLE line 2: 2 30395 98.9387 207.6721 0161780 103.9455 22.9350 13.96436856938025
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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