Key statistics
Satellite CZ-4C R/B at a glance.
Uptime
4243
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 2013-052B
Object number (NORAD): 39261
Object ID (CCSDS): 39261
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 100.43 minutes
Inclination: 98.895 deg
SMA: 7157.072 km
Apoapsis: 801.115 km
Periapsis: 756.76 km
RAAN: 359.0564 deg
Eccentricy: 0.0030987
Argument of periapsis: 207.8187 deg
Mean anomaly: 152.134 deg
Mean motion: 14.33836597 rev/day
Mean motion (dot): 0.00000112 rev/day2
B* drag term: 0.000056776 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 10:19 p.m. UTC
TLE line 0: 0 CZ-4C R/B
TLE line 1: 1 39261U 13052B 25125.93022886 .00000112 00000-0 56776-4 0 9994
TLE line 2: 2 39261 98.8950 359.0564 0030987 207.8187 152.1340 14.33836597607350
Live tracking on map
Real-time ground track for satellite CZ-4C R/B.
In-orbit conjunctions
A list of the most updated potential collisions computed for object CZ-4C R/B.
Associated space launch
CZ-4C R/B was lifted into orbit during the mission ‘Long March 4C | Fengyun-3C’, on board a Long March 4C space rocket.
The launch took place on Sept. 23, 2013, 3:07 a.m. from Launch Complex 9.
For more information about the launch, click the button.
Long March 4C | Fengyun-3C
Agency: N/A
Status: Launch Successful
Launch date: Sept. 23, 2013, 3:07 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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