Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025EEC
Object number (NORAD): 37044
Object ID (CCSDS): 37044
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.262 minutes
Inclination: 98.9537 deg
SMA: 7384.859 km
Apoapsis: 1386.566 km
Periapsis: 626.881 km
RAAN: 244.2449 deg
Eccentricy: 0.0514353
Argument of periapsis: 31.0071 deg
Mean anomaly: 332.0392 deg
Mean motion: 13.68010593 rev/day
Mean motion (dot): 0.00006847 rev/day2
B* drag term: 0.0031947 1/REarth
Two-line elements (TLE)
Creation date: May 3, 2025, 5:28 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 3, 2025, 1:12 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37044U 99025EEC 25123.55008360 .00006847 00000-0 31947-2 0 9994
TLE line 2: 2 37044 98.9537 244.2449 0514353 31.0071 332.0392 13.68010593808041
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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