Key statistics
Satellite CZ-2C R/B at a glance.
Uptime
225
Days in orbit
Revolutions
≈ 15.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.5
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-2C R/B.
Object identification
Identified? True
Debris? False
Object name: CZ-2C R/B
International designator: 2024-218A
Object number (NORAD): 62078
Object ID (CCSDS): 62078
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 94.809 minutes
Inclination: 97.5453 deg
SMA: 6887.466 km
Apoapsis: 544.523 km
Periapsis: 474.139 km
RAAN: 197.6607 deg
Eccentricy: 0.0051096
Argument of periapsis: 134.1699 deg
Mean anomaly: 226.3753 deg
Mean motion: 15.18845373 rev/day
Mean motion (dot): 0.00004921 rev/day2
B* drag term: 0.00023161 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 11:06 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 9:52 p.m. UTC
TLE line 0: 0 CZ-2C R/B
TLE line 1: 1 62078U 24218A 25187.91123119 .00004921 00000-0 23161-3 0 9992
TLE line 2: 2 62078 97.5453 197.6607 0051096 134.1699 226.3753 15.18845373 33951
Live tracking on map
Real-time ground track for satellite CZ-2C R/B.
Associated space launch
Commercial Synthetic-aperture radar Earth observation satellites built by CAST for China Siwei Survey and Mapping Technology Co. Ltd.
CZ-2C R/B was lifted into orbit during the mission ‘Long March 2C | SuperView Neo 2-03 & 04’, on board a Long March 2 space rocket.
The launch took place on Nov. 24, 2024, 11:39 p.m. from Launch Area 4 (SLS-2 / 603).
For more information about the launch, click the button.
Long March 2C | SuperView Neo 2-03 & 04
Agency: N/A
Status: Launch Successful
Launch date: Nov. 24, 2024, 11:39 p.m. UTC
Rocket: Long March 2
Launch pad: Launch Area 4 (SLS-2 / 603)
Location: Jiuquan Satellite Launch Center, People's Republic of China
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