Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 13.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025CRV
Object number (NORAD): 32127
Object ID (CCSDS): 32127
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.957 minutes
Inclination: 99.2415 deg
SMA: 7417.315 km
Apoapsis: 1248.134 km
Periapsis: 830.225 km
RAAN: 80.9565 deg
Eccentricy: 0.0281712
Argument of periapsis: 232.0785 deg
Mean anomaly: 125.4587 deg
Mean motion: 13.59041422 rev/day
Mean motion (dot): 0.0000227 rev/day2
B* drag term: 0.0024257 1/REarth
Two-line elements (TLE)
Creation date: May 2, 2025, 2:33 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 23, 2025, 3:21 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32127U 99025CRV 25113.13964968 .00002270 00000-0 24257-2 0 9991
TLE line 2: 2 32127 99.2415 80.9565 0281712 232.0785 125.4587 13.59041422572476
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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