Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 13.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025GV
Object number (NORAD): 29899
Object ID (CCSDS): 29899
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 107.671 minutes
Inclination: 98.6498 deg
SMA: 7497.091 km
Apoapsis: 1382.918 km
Periapsis: 854.994 km
RAAN: 315.6952 deg
Eccentricy: 0.0352086
Argument of periapsis: 269.2085 deg
Mean anomaly: 86.8699 deg
Mean motion: 13.37406988 rev/day
Mean motion (dot): 0.00000163 rev/day2
B* drag term: 0.00026822 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 11:15 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29899U 99025GV 25127.96886762 .00000163 00000-0 26822-3 0 9994
TLE line 2: 2 29899 98.6498 315.6952 0352086 269.2085 86.8699 13.37406988891609
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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