Starlink v1.0 13-1/60

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 46670/46729 - 20073A/073BM
Launch date 18 Oct 2020 - UTC
Launch site CCK, SLC39A
Launch vehicle  Falcon-9 v1.2 (Block 5)
Mission Communication, Internet
Earth orbit:
Perigee / Apogee 553 x 555 km
Inclination 53.1°
Period 95.6 min

60 satellites launched together (see table).

 Satellite  Cospar nº  Int. Design.  Orbit  Decay
 Starlink v1.0 13-1 (1819)  2020-073A  46670    25 Oct 2020 (.10)
 Starlink v1.0 13-2 (1715)  2020-073B  46671  553.5 x 555.2 x 53.1  
 Starlink v1.0 13-3 (1716)  2020-073C  46672    
 Starlink v1.0 13-4 (1717)  2020-073D  46673    
 Starlink v1.0 13-5 (1718)  2020-073E  46674    
 Starlink v1.0 13-6 (1720)  2020-073F  46675    
 Starlink v1.0 13-7 (1731)  2020-073G  46676    
 Starlink v1.0 13-8 (1766)  2020-073H  46677    
 Starlink v1.0 13-9 (1772)  2020-073J  46678    27 Dec 2020 (.58)
 Starlink v1.0 13-10 (1773)  2020-073K  46679    
 Starlink v1.0 13-11 (1774)  2020-073L  46680    
 Starlink v1.0 13-12 (1775)  2020-073M  46681    
 Starlink v1.0 13-13 (1776)  2020-073N  46682    
 Starlink v1.0 13-14 (1778)  2020-073P  46683    
 Starlink v1.0 13-15 (1780)  2020-073Q  46684    
 Starlink v1.0 13-16 (1781)  2020-073R  46685    
 Starlink v1.0 13-17 (1783)  2020-073S  46686    
 Starlink v1.0 13-18 (1784)  2020-073T  46687    
 Starlink v1.0 13-19 (1786)  2020-073U  46688    
 Starlink v1.0 13-20 (1788)  2020-073V  46689    
 Starlink v1.0 13-21 (1789)  2020-073W  46690    
 Starlink v1.0 13-22 (1790)  2020-073X  46691    
 Starlink v1.0 13-23 (1791)  2020-073Y  46692    
 Starlink v1.0 13-24 (1792)  2020-073Z  46693    
 Starlink v1.0 13-25 (1793)  2020-073AA  46694    
 Starlink v1.0 13-26 (1794)  2020-073AB  46695    
 Starlink v1.0 13-27 (1795)  2020-073AC  46696    
 Starlink v1.0 13-28 (1796)  2020-073AD  46697    
 Starlink v1.0 13-29 (1797)  2020-073AE  46698    
 Starlink v1.0 13-30 (1799)  2020-073AF  46699    
 Starlink v1.0 13-31 (1800)  2020-073AG  46700    
 Starlink v1.0 13-32 (1801)  2020-073AH  46701    
 Starlink v1.0 13-33 (1802)  2020-073AJ  46702    
 Starlink v1.0 13-34 (1803)  2020-073AK  46703    
 Starlink v1.0 13-35 (1804)  2020-073AL  46704    
 Starlink v1.0 13-36 (1805)  2020-073AM  46705    
 Starlink v1.0 13-37 (1807)  2020-073AN  46706    
 Starlink v1.0 13-38 (1808)  2020-073AP  46707    
 Starlink v1.0 13-39(1809)  2020-073AQ  46708    
 Starlink v1.0 13-40 (1810)  2020-073AR  46709    
 Starlink v1.0 4-41(1811)  2020-073AS  46710    
 Starlink v1.0 13-42 (1813)  2020-073AT  46711    
 Starlink v1.0 13-43 (1814)  2020-073AU  46712    
 Starlink v1.0 13-44 (1815)  2020-073AV  46713    
 Starlink v1.0 13-45 (1816)  2020-073AW  46714    
 Starlink v1.0 13-46 (1817)  2020-073AX  46715    
 Starlink v1.0 13-47 (1818)  2020-073AY  46716    
 Starlink v1.0 13-48 (1820)  2020-073AZ  46717    
 Starlink v1.0 13-49 (1821)  2020-073BA  46718    
 Starlink v1.0 13-50 (1822)  2020-073BB  46719    
 Starlink v1.0 13-51 (1823)  2020-073BC  46720    
 Starlink v1.0 13-52 (1824)  2020-073BD  46721    
 Starlink v1.0 13-53 (1825)  2020-073BE  46722    
 Starlink v1.0 13-54 (1826)  2020-073BF  46723    
 Starlink v1.0 13-55 (1827)  2020-073BG  46724    
 Starlink v1.0 13-56 (1828)  2020-073BH  46725    
 Starlink v1.0 13-57 (1829)  2020-073BJ  46726    
 Starlink v1.0 13-58 (1830)  2020-073BK  46727    
 Starlink v1.0 13-59 (1831)  2020-073BL  46728    
 Starlink v1.0 13-60 (1841)  2020-073BM  46729    

Spacecraft data:

Prime manufacturer SpaceX
Platform 
Operator SpaceX
Mass at launch  227 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment Ku/Ka-band payload, optical inter-satellite link
Solar array Solar arrays
Stabilization  
Propulsion 
DC power  
Design lifetime  


Description:

  • Starlink is SpaceX′s 4425-satellites low earth orbit constellation to provide broadband Internet access.
  • The mass-produced spacecraft carry a communications payload using the Ku and Ka frequency bands. The satellites will employ optical inter-satellite links and phased array beam forming and digital processing technologies.
  • The Starlink satellites feature a flat panel design with a single solar panel and have a mass of about 227 kg. The satellites are stacked for launch without the need for an dispenser. As a propulsion system for orbit adjustion and maintenance as well as deorbiting, they use krypton-fueled Hall thrusters. The Startracker navigation system is based on the heritage of Dragon. The satellites are designed autonomously avoid collisions based on uplinked tracking data. At the end of life, the Starlink satellites are to be actively deorbited, leading to reentry. 95% of the material is expected to burn up.
  • The first 1584 Starlink satellites are to operate from a 550 km orbit. Later sub-constellations are planned for 1200 km and very low 340 km orbital altitude, bringing the final constellation size to nearly 12000 satellites.
  • The initial 75 satellites, called Block v0.9, are prototypes without inter-satellite links and Ka-band antennas. These are to be used for extensive testing of deployment and operation and also of deliberate deorbiting.
  • For launch, 60 satellites are stacked on top of each other without the need of a massive deployer. 60 satellite is the maximum possible to fit inside the Falcon-9 v1.2 (Block 5), although a future enlarged fairing will allow launches of more than 60 satellites per mission.

Mission details:

External links:


Ref.: #3(SD576,578), #7(JR), #228 - update: 15.04.21 Home