Starlink v1.0 11-1/60

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 46325/46385 - 20062A/062BM
Launch date 03 Sep 2020 - 12:46 UTC
Launch site CCK, LC39A
Launch vehicle  Falcon-9 v1.2 (Block 5)
Mission Communication, Internet
Earth orbit:
Perigee / Apogee 552 x 556 km
Inclination 53.1°
Period 95.6 min

60 satellites launched together (see table).

 Satellite  Cospar nº  Int. Design.  Orbit  Decay
 Starlink v1.0 11-1 (1734)  2020-062A  46325  552.6 x 556.1 x 53.1  
 Starlink v1.0 11-2 (1654)  2020-062B  46326    
 Starlink v1.0 11-3 (1673)  2020-062C  46327    
 Starlink v1.0 11-4 (1686)  2020-062D  46328    
 Starlink v1.0 11-5 (1695)  2020-062E  46329    
 Starlink v1.0 11-6 (1710)  2020-062F  46330    
 Starlink v1.0 11-7 (1719)  2020-062G  46331    
 Starlink v1.0 11-8 (1721)  2020-062H  46332    
 Starlink v1.0 11-9 (1723)  2020-062J  46333    
 Starlink v1.0 11-10 (1725)  2020-062K  46334    
 Starlink v1.0 11-11 (1727)  2020-062L  46335    
 Starlink v1.0 11-12 (1738)  2020-062M  46336    
 Starlink v1.0 11-13 (1750)  2020-062N  46337    
 Starlink v1.0 11-14 (1752)  2020-062P  46338    
 Starlink v1.0 11-15 (1757)  2020-062Q  46339    
 Starlink v1.0 11-16 (1759)  2020-062R  46340    
 Starlink v1.0 11-17 (1760)  2020-062S  46341    
 Starlink v1.0 11-18 (1762)  2020-062T  46342    
 Starlink v1.0 11-19 (1764)  2020-062U  46343    
 Starlink v1.0 11-20 (1765)  2020-062V  46344    
 Starlink v1.0 11-21 (1767)  2020-062W  46345    
 Starlink v1.0 11-22 (1546)  2020-062X  46346    
 Starlink v1.0 11-23 (1547)  2020-062Y  46347    
 Starlink v1.0 11-24 (1553)  2020-062Z  46348    
 Starlink v1.0 11-25 (1575)  2020-062AA  46349    
 Starlink v1.0 11-26 (1617)  2020-062AB  46350    
 Starlink v1.0 11-27 (1646)  2020-062AC  46351    
 Starlink v1.0 11-28 (1653)  2020-062AD  46352    
 Starlink v1.0 11-29 (1656)  2020-062AE  46353    
 Starlink v1.0 11-30 (1657)  2020-062AF  46354    
 Starlink v1.0 11-31 (1661)  2020-062AG  46355    
 Starlink v1.0 11-32 (1665)  2020-062AH  46356    
 Starlink v1.0 11-33 (1666)  2020-062AJ  46357    
 Starlink v1.0 11-34 (1690)  2020-062AK  46358    
 Starlink v1.0 11-35 (1707)  2020-062AL  46359    
 Starlink v1.0 11-36 (1713)  2020-062AM  46360    
 Starlink v1.0 11-37 (1722)  2020-062AN  46361    
 Starlink v1.0 11-38 (1726)  2020-062AP  46362    
 Starlink v1.0 11-39(1739)  2020-062AQ  46363    
 Starlink v1.0 11-40 (1763)  2020-062AR  46364    
 Starlink v1.0 4-41(1550)  2020-062AS  46365    
 Starlink v1.0 11-42 (1651)  2020-062AT  46366    
 Starlink v1.0 11-43 (1652)  2020-062AU  46367    
 Starlink v1.0 11-44 (1658)  2020-062AV  46368    
 Starlink v1.0 11-45 (1662)  2020-062AW  46369    
 Starlink v1.0 11-46 (1670)  2020-062AX  46370    
 Starlink v1.0 11-47 (1688)  2020-062AY  46371    
 Starlink v1.0 11-48 (1689)  2020-062AZ  46372    
 Starlink v1.0 11-49(1691)  2020-062BA  46373    
 Starlink v1.0 11-50 (1711)  2020-062BB  46374    
 Starlink v1.0 11-51 (1724)  2020-062BC  46375    
 Starlink v1.0 11-52 (1742)  2020-062BD  46376  551.9 x 556.8 x 53.1  
 Starlink v1.0 11-53 (1745)  2020-062BE  46377  553.0 x 555.7 x 53.1  
 Starlink v1.0 11-54 (1751)  2020-062BF  46378  552.9 x 555.9 x 53.1  
 Starlink v1.0 11-55 (1756)  2020-062BG  46379  373.5 x 384.3 x 53.0  
 Starlink v1.0 11-56 (1758)  2020-062BH  46380  552.6 x 556.1 x 53.1  
 Starlink v1.0 11-57 (1768)  2020-062BJ  46381  433.2 x 443.4 x 53.1  
 Starlink v1.0 11-58 (1769)  2020-062BK  46382  553.1 x 555.6 x 53.1  
 Starlink v1.0 11-59 (1770)  2020-062BL  46383  552.6 x 556.2 x 53.1  
 Starlink v1.0 11-60 (1771)  2020-062BM  46384  552.3 x 556.5 x 53.1  

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:

  • The 12th Starlink launch (V1.0-L11) on Sep 3, 202 carried 60 more Starlinks into orbit.

External links:


Ref.: #7(JR783), - update: 20.01.21 Home