Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9612
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025GH
Object number (NORAD): 29887
Object ID (CCSDS): 29887
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.506 minutes
Inclination: 98.725 deg
SMA: 7160.696 km
Apoapsis: 989.805 km
Periapsis: 575.317 km
RAAN: 325.2269 deg
Eccentricy: 0.02894186
Argument of periapsis: 300.3649 deg
Mean anomaly: 71.5589 deg
Mean motion: 14.32748317 rev/day
Mean motion (dot): 0.00002753 rev/day2
B* drag term: 0.000647627 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 7:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 1, 2025, 12:05 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29887U 99025GH 25244.50353574 .00002753 00000-0 64763-3 0 9994
TLE line 2: 2 29887 98.7250 325.2269 0289419 300.3649 71.5589 14.32748317965100
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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