Starlink v1.0 14-1/60

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 46739/46798 - 20074A/074BM
Launch date 24 Oct 2020 - UTC
Launch site CCAFS, SLC-40
Launch vehicle  Falcon-9 v1.2 (B5) (B1060.3)
Mission Communication, Internet
Earth orbit:
Perigee / Apogee 498 x 505 km
Inclination 53.1°
Period 94.5 min

60 satellites launched together (see table).

 Satellite  Cospar nº  Int. Design.  Orbit  Decay
 Starlink v1.0 14-1 (1847)  2020-074A  46739  498.7 x 504.8 x 53.1  
 Starlink v1.0 14-2 (1848)  2020-074B  46740    
 Starlink v1.0 14-3 (1865)  2020-074C  46741    
 Starlink v1.0 14-4 (1872)  2020-074D  46742    
 Starlink v1.0 14-5 (1892)  2020-074E  46743    
 Starlink v1.0 14-6 (1894)  2020-074F  46744    
 Starlink v1.0 14-7 (1898)  2020-074G  46745    
 Starlink v1.0 14-8 (1905)  2020-074H  46746    
 Starlink v1.0 14-9 (1908)  2020-074J  46747    
 Starlink v1.0 14-10 (1910)  2020-074K  46748    
 Starlink v1.0 14-11 (1911)  2020-074L  46749    
 Starlink v1.0 14-12 (1915)  2020-074M  46750    06 Nov 2020 (.5)
 Starlink v1.0 14-13 (1920)  2020-074N  46751    
 Starlink v1.0 14-14 (1921)  2020-074P  46752    
 Starlink v1.0 14-15 (1922)  2020-074Q  46753    
 Starlink v1.0 14-16 (1923)  2020-074R  46754    
 Starlink v1.0 14-17 (1924)  2020-074S  46755    
 Starlink v1.0 14-18 (1925)  2020-074T  46756    
 Starlink v1.0 14-19 (1926)  2020-074U  46757    
 Starlink v1.0 14-20 (1928)  2020-074V  46758    
 Starlink v1.0 14-21 (1833)  2020-074W  46759    
 Starlink v1.0 14-22 (1896)  2020-074X  46760    
 Starlink v1.0 14-23 (1897)  2020-074Y  46761    
 Starlink v1.0 14-24 (1901)  2020-074Z  46762    
 Starlink v1.0 14-25 (1902)  2020-074AA  46763    
 Starlink v1.0 14-26 (1903)  2020-074AB  46764    
 Starlink v1.0 14-27 (1906)  2020-074AC  46765    
 Starlink v1.0 14-28 (1916)  2020-074AD  46766    
 Starlink v1.0 14-29 (1917)  2020-074AE  46767    
 Starlink v1.0 14-30 (1918)  2020-074AF  46768    
 Starlink v1.0 14-31 (1919)  2020-074AG  46769    
 Starlink v1.0 14-32 (1932)  2020-074AH  46770    
 Starlink v1.0 14-33 (1935)  2020-074AJ  46771    
 Starlink v1.0 14-34 (1936)  2020-074AK  46772    
 Starlink v1.0 14-35 (1937)  2020-074AL  46773    
 Starlink v1.0 14-36 (1939)  2020-074AM  46774    
 Starlink v1.0 14-37 (1945)  2020-074AN  46775    
 Starlink v1.0 14-38 (1946)  2020-074AP  46776    
 Starlink v1.0 14-39 (1949)  2020-074AQ  46777    
 Starlink v1.0 14-40 (1950)  2020-074AR  46778    06 Nov 2020 (.63)
 Starlink v1.0 14-41 (1798)  2020-074AS  46779    
 Starlink v1.0 14-42 (1832)  2020-074AT  46780    
 Starlink v1.0 14-43 (1834)  2020-074AU  46781    
 Starlink v1.0 14-44 (1835)  2020-074AV  46782    
 Starlink v1.0 14-45 (1851)  2020-074AW  46783    
 Starlink v1.0 14-46 (1882)  2020-074AX  46784    
 Starlink v1.0 14-47 (1883)  2020-074AY  46784    
 Starlink v1.0 14-48 (1893)  2020-074AZ  46786    
 Starlink v1.0 14-49 (1899)  2020-074BA  46787    
 Starlink v1.0 14-50 (1929)  2020-074BB  46788    
 Starlink v1.0 14-51 (1930)  2020-074BC  46789    
 Starlink v1.0 14-52 (1931)  2020-074BD  46790    
 Starlink v1.0 14-53 (1933)  2020-074BE  46791    
 Starlink v1.0 14-54 (1934)  2020-074BF  46792    
 Starlink v1.0 14-55 (1941)  2020-074BG  46793    
 Starlink v1.0 14-56 (1942)  2020-074BH  46794    
 Starlink v1.0 14-57 (1943)  2020-074BJ  46795    
 Starlink v1.0 14-58 (1944)  2020-074BK  46796    
 Starlink v1.0 14-59 (1947)  2020-074BL  46797    
 Starlink v1.0 14-60 (1948)  2020-074BM  46798    

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(SD577), #7(JR), #228 - update: 14.03.21 Home