XC 1-4(Xingchen 1-4)

China

Spacecraft nº:

Chinese spacecraft nº: 268 - 271

Launch data:

Designation 15049
Launch date 19 Sep 2015 - 23:01 UT
Launch site Taiyuan, LC-16
Launch vehicle  CZ-6
Mission Technology
Earth orbit:
Perigee / Apogee  km
Eccentricity 
Inclination  °
Period  min

Launched together with: XY 2 - DCBB - ZDPS 2A & 2B - XW 2A-2F - LilacSat 2 - NS 2 - ZJ 1 - KJSY 1 - TT 3 - NUDT-PhoneSat

Spacecraft data:

Prime manufacturer 
Platform 
Operator 
Mass at launch   kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment 
Solar array Solar cells
Stabilization  
Propulsion None
DC power  
Design lifetime  

 XC 1XC 2XC 3XC 4
Norad ID - - - -
Int. code 15049 15049 15019 15049
Earth orbit
Perigee / Apogee 515 x 536 km 515 x 536 km 515 x 536 km 515 x 536 km
Inclination 97.5 deg 97.5 deg 97.5 deg 97.5 deg
Period  min  min  min  min
Decay     


Ref.: #7(JR716) - update: 29.01.16 Home