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
98.5
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: 1999-025ZG
Object number (NORAD): 30295
Object ID (CCSDS): 30295
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.061 minutes
Inclination: 98.5215 deg
SMA: 7187.034 km
Apoapsis: 876.131 km
Periapsis: 741.666 km
RAAN: 214.1811 deg
Eccentricy: 0.0093547
Argument of periapsis: 188.0817 deg
Mean anomaly: 204.2426 deg
Mean motion: 14.24879778 rev/day
Mean motion (dot): 0.00000242 rev/day2
B* drag term: 0.0001162 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, 12:57 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30295U 99025ZG 25187.03972684 .00000242 00000-0 11620-3 0 9997
TLE line 2: 2 30295 98.5215 214.1811 0093547 188.0817 204.2426 14.24879778959022
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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