Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
6499
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4 DEB.
Object identification
Identified? True
Debris? True
Object name: CZ-4 DEB
International designator: 2007-042G
Object number (NORAD): 35567
Object ID (CCSDS): 35567
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.537 minutes
Inclination: 98.8344 deg
SMA: 7209.555 km
Apoapsis: 842.964 km
Periapsis: 819.876 km
RAAN: 134.8558 deg
Eccentricy: 0.0016012
Argument of periapsis: 116.3371 deg
Mean anomaly: 243.945 deg
Mean motion: 14.18208388 rev/day
Mean motion (dot): 0.00000482 rev/day2
B* drag term: 0.00025571 1/REarth
Two-line elements (TLE)
Creation date: June 29, 2025, 5:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 29, 2025, 3:40 a.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 35567U 07042G 25180.15278096 .00000482 00000-0 25571-3 0 9990
TLE line 2: 2 35567 98.8344 134.8558 0016012 116.3371 243.9450 14.18208388612739
Live tracking on map
Real-time ground track for satellite CZ-4 DEB.
Associated space launch
Chinese-Brazilian Earth observation satellite
CZ-4 DEB was lifted into orbit during the mission ‘Long March 4B | Zi Yuan 1-2B’, on board a Long March 4B space rocket.
The launch took place on Sept. 19, 2007, 3:26 a.m. from Launch Complex 7.
For more information about the launch, click the button.
Long March 4B | Zi Yuan 1-2B
Agency: N/A
Status: Launch Successful
Launch date: Sept. 19, 2007, 3:26 a.m. UTC
Rocket: Long March 4B
Launch pad: Launch Complex 7
Location: Taiyuan Satellite Launch Center, People's Republic of China
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