Key statistics
Satellite CZ-4B DEB at a glance.
Uptime
6190
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4B DEB.
Object identification
Identified? True
Debris? True
Object name: CZ-4B DEB
International designator: 2008-026C
Object number (NORAD): 37571
Object ID (CCSDS): 37571
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.592 minutes
Inclination: 98.8901 deg
SMA: 7353.49 km
Apoapsis: 1153.278 km
Periapsis: 797.432 km
RAAN: 201.5869 deg
Eccentricy: 0.0241957
Argument of periapsis: 290.083 deg
Mean anomaly: 67.4432 deg
Mean motion: 13.76773603 rev/day
Mean motion (dot): 0.0000049 rev/day2
B* drag term: 0.00043642 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, 10:31 a.m. UTC
TLE line 0: 0 CZ-4B DEB
TLE line 1: 1 37571U 08026C 25127.43884730 .00000490 00000-0 43642-3 0 9998
TLE line 2: 2 37571 98.8901 201.5869 0241957 290.0830 67.4432 13.76773603646703
Live tracking on map
Real-time ground track for satellite CZ-4B DEB.
Associated space launch
Chinese 2nd generation polar orbiting meteorological satellite
CZ-4B DEB was lifted into orbit during the mission ‘Long March 4C | Feng Yun 3A’, on board a Long March 4C space rocket.
The launch took place on May 27, 2008, 3:02 a.m. from Launch Complex 7.
For more information about the launch, click the button.

Long March 4C | Feng Yun 3A
Agency: N/A
Status: Launch Successful
Launch date: May 27, 2008, 3:02 a.m. UTC
Rocket: Long March 4C
Launch pad: Launch Complex 7
Location: Taiyuan Satellite Launch Center, People's Republic of China
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