Key statistics
Satellite CZ-4C DEB at a glance.
Uptime
3622
Days in orbit
Revolutions
≈ 15.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.3
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4C DEB.
Object identification
Identified? True
Debris? True
Object name: CZ-4C DEB
International designator: 2015-069E
Object number (NORAD): 42672
Object ID (CCSDS): 42672
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 96.315 minutes
Inclination: 98.2703 deg
SMA: 6960.222 km
Apoapsis: 643.418 km
Periapsis: 520.757 km
RAAN: 269.774 deg
Eccentricy: 0.0088116
Argument of periapsis: 9.2612 deg
Mean anomaly: 351.0207 deg
Mean motion: 14.95092609 rev/day
Mean motion (dot): 0.00027787 rev/day2
B* drag term: 0.0023441609 1/REarth
Two-line elements (TLE)
Creation date: Oct. 26, 2025, 2:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 25, 2025, 9:16 p.m. UTC
TLE line 0: 0 CZ-4C DEB
TLE line 1: 1 42672U 15069E 25298.88629256 .00027787 00000-0 23442-2 0 9992
TLE line 2: 2 42672 98.2703 269.7740 0088116 9.2612 351.0207 14.95092609523981
Live tracking on map
Real-time ground track for satellite CZ-4C DEB.
Associated space launch
CZ-4C DEB was lifted into orbit during the mission ‘Long March 4C | Yaogan-29’, on board a Long March 4C space rocket.
The launch took place on Nov. 26, 2015, 9:24 p.m. from Launch Complex 9.
For more information about the launch, click the button.
Long March 4C | Yaogan-29
Agency: N/A
Status: Launch Successful
Launch date: Nov. 26, 2015, 9:24 p.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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