Starlink v1.0 L19-1/60

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 47620/47679 - 21012A/012BM
Launch date 16 Feb 2021 - UTC
Launch site CCK, SLC40
Launch vehicle  Falcon-9 v1.2 (Block 5)
Mission Communication, Internet
Earth orbit:
Perigee / Apogee 386 x 388 km
Inclination 53.1°
Period 92.2 min

60 satellites launched together (see table).

 Satellite  Cospar nº  Int. Design.  Orbit  Decay
 Starlink v1.0 L19-1 (1528)  2021-012A  47620  386.9 x 388.6 x 53.1  
 Starlink v1.0 L19-2 (1609)  2021-012B  47621    
 Starlink v1.0 L19-3 (1645)  2021-012C  47622    
 Starlink v1.0 L19-4 (1655)  2021-012D  47623    
 Starlink v1.0 L19-5 (1669)  2021-012E  47624    
 Starlink v1.0 L19-6 (1704)  2021-012F  47625    
 Starlink v1.0 L19-7 (1761)  2021-012G  47626    
 Starlink v1.0 L19-8 (1972)  2021-012H  47627    
 Starlink v1.0 L19-9 (1973)  2021-012J  47628    
 Starlink v1.0 L19-10 (1974)  2021-012K  47629    
 Starlink v1.0 L19-11 (1983)  2021-012L  47630    
 Starlink v1.0 L19-12 (1985)  2021-012M  47631    
 Starlink v1.0 L19-13 (1992)  2021-012N  47632    
 Starlink v1.0 L19-14 (2009)  2021-012P  47633    
 Starlink v1.0 L19-15 (2010)  2021-012Q  47634    
 Starlink v1.0 L19-16 (2012)  2021-012R  47635    
 Starlink v1.0 L19-17 (2013)  2021-012S  47636    
 Starlink v1.0 L19-18 (2014)  2021-012T  47637    
 Starlink v1.0 L19-19 (2015)  2021-012U  47638    
 Starlink v1.0 L19-20 (2016)  2021-012V  47639    
 Starlink v1.0 L19-21 (2018)  2021-012W  47640    
 Starlink v1.0 L19-22 (2019)  2021-012X  47641    
 Starlink v1.0 L19-23 (2020)  2021-012Y  47642    
 Starlink v1.0 L19-24 (2022)  2021-012Z  47643    
 Starlink v1.0 L19-25 (2026)  2021-012AA  47644    
 Starlink v1.0 L19-26 (2027)  2021-012AB  47645    
 Starlink v1.0 L19-27 (2028)  2021-012AC  47646    
 Starlink v1.0 L19-28 (2030)  2021-012AD  47647    
 Starlink v1.0 L19-29 (2031)  2021-012AE  47648    
 Starlink v1.0 L19-30 (2032)  2021-012AF  47649    
 Starlink v1.0 L19-31 (2033)  2021-012AG  47650    
 Starlink v1.0 L19-32 (2035)  2021-012AH  47651    
 Starlink v1.0 L19-33 (2036)  2021-012AJ  47652    
 Starlink v1.0 L19-34 (2037)  2021-012AK  47653    
 Starlink v1.0 L19-35 (2038)  2021-012AL  47654    
 Starlink v1.0 L19-36 (2039)  2021-012AM  47655    
 Starlink v1.0 L19-37 (2040)  2021-012AN  47656    
 Starlink v1.0 L19-38 (2041)  2021-012AP  47657    
 Starlink v1.0 L19-39 (2042)  2021-012AQ  47658    
 Starlink v1.0 L19-40 (2043)  2021-012AR  47659    
 Starlink v1.0 L19-41 (2044)  2021-012AS  47660    
 Starlink v1.0 L19-42 (2051)  2021-012AT  47661    
 Starlink v1.0 L19-43 (2052)  2021-012AU  47662    
 Starlink v1.0 L19-44 (2053)  2021-012AV  47663    
 Starlink v1.0 L19-45 (2054)  2021-012AW  47664    
 Starlink v1.0 L19-46 (2056)  2021-012AX  47665    
 Starlink v1.0 L19-47 (2057)  2021-012AY  47666    
 Starlink v1.0 L19-48 (2058)  2021-012AZ  47667    
 Starlink v1.0 L19-49 (2059)  2021-012BA  47668    
 Starlink v1.0 L19-50 (2060)  2021-012BB  47669    
 Starlink v1.0 L19-51 (2062)  2021-012BC  47670    
 Starlink v1.0 L19-52 (2064)  2021-012BD  47671    
 Starlink v1.0 L19-53 (2065)  2021-012BE  47672    
 Starlink v1.0 L19-54 (2066)  2021-012BF  47673    
 Starlink v1.0 L19-55 (2067)  2021-012BG  47674    
 Starlink v1.0 L19-56 (2078)  2021-012BH  47675    
 Starlink v1.0 L19-57 (2083)  2021-012BJ  47676    
 Starlink v1.0 L19-58 (2090)  2021-012BK  47677    
 Starlink v1.0 L19-59 (2091)  2021-012BL  47678    
 Starlink v1.0 L19-60 (2095)  2021-012BM  47679    

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.

Mission details:

External links:


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