Key statistics
Satellite CZ-4B R/B at a glance.
Uptime
3929
Days in orbit
Revolutions
≈ 15.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.5
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4B R/B.
Object identification
Identified? True
Debris? False
Object name: CZ-4B R/B
International designator: 2014-079B
Object number (NORAD): 40337
Object ID (CCSDS): 40337
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 95.803 minutes
Inclination: 98.4897 deg
SMA: 6935.552 km
Apoapsis: 659.612 km
Periapsis: 455.223 km
RAAN: 314.4294 deg
Eccentricy: 0.01473485
Argument of periapsis: 194.2238 deg
Mean anomaly: 165.4816 deg
Mean motion: 15.03076785 rev/day
Mean motion (dot): 0.00005202 rev/day2
B* drag term: 0.00030914245 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 9:49 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 4:48 a.m. UTC
TLE line 0: 0 CZ-4B R/B
TLE line 1: 1 40337U 14079B 25251.20049161 .00005202 00000-0 30914-3 0 9995
TLE line 2: 2 40337 98.4897 314.4294 0147349 194.2238 165.4816 15.03076785585324
Live tracking on map
Real-time ground track for satellite CZ-4B R/B.
Associated space launch
CZ-4B R/B was lifted into orbit during the mission ‘Long March 4B | CBERS-4’, on board a Long March 4B space rocket.
The launch took place on Dec. 7, 2014, 3:26 a.m. from Launch Complex 9.
For more information about the launch, click the button.
Long March 4B | CBERS-4
Agency: N/A
Status: Launch Successful
Launch date: Dec. 7, 2014, 3:26 a.m. UTC
Rocket: Long March 4B
Launch pad: Launch Complex 9
Location: Taiyuan Satellite Launch Center, People's Republic of China
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