Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.6
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: 1999-025CU
Object number (NORAD): 29802
Object ID (CCSDS): 29802
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.904 minutes
Inclination: 98.6133 deg
SMA: 7084.395 km
Apoapsis: 735.035 km
Periapsis: 677.484 km
RAAN: 228.9311 deg
Eccentricy: 0.0040618
Argument of periapsis: 291.1137 deg
Mean anomaly: 189.8574 deg
Mean motion: 14.5595726 rev/day
Mean motion (dot): 0.00008658 rev/day2
B* drag term: 0.0019571 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 7:58 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29802U 99025CU 25127.83223806 .00008658 00000-0 19571-2 0 9997
TLE line 2: 2 29802 98.6133 228.9311 0040618 291.1137 189.8574 14.55957260952824
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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