Key statistics
Satellite CZ-4C R/B at a glance.
Uptime
4073
Days in orbit
Revolutions
≈ 13.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
100.2
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4C R/B.
Object identification
Identified? True
Debris? False
Object name: CZ-4C R/B
International designator: 2014-063B
Object number (NORAD): 40276
Object ID (CCSDS): 40276
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 107.221 minutes
Inclination: 100.2287 deg
SMA: 7476.17 km
Apoapsis: 1204.655 km
Periapsis: 991.416 km
RAAN: 265.9267 deg
Eccentricy: 0.01426124
Argument of periapsis: 340.9728 deg
Mean anomaly: 18.6106 deg
Mean motion: 13.43024718 rev/day
Mean motion (dot): 0.00000002 rev/day2
B* drag term: 0.000081287427 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 3:36 p.m. UTC
TLE line 0: 0 CZ-4C R/B
TLE line 1: 1 40276U 14063B 25347.65006860 .00000002 00000-0 81287-4 0 9997
TLE line 2: 2 40276 100.2287 265.9267 0142612 340.9728 18.6106 13.43024718546603
Live tracking on map
Real-time ground track for satellite CZ-4C R/B.
Associated space launch
CZ-4C R/B was lifted into orbit during the mission ‘Long March 4C | Yaogan-22’, on board a Long March 4C space rocket.
The launch took place on Oct. 20, 2014, 6:31 a.m. from Launch Complex 9.
For more information about the launch, click the button.
Long March 4C | Yaogan-22
Agency: N/A
Status: Launch Successful
Launch date: Oct. 20, 2014, 6:31 a.m. UTC
Rocket: Long March 4C
Launch pad: Launch Complex 9
Location: Taiyuan Satellite Launch Center, People's Republic of China
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