Starlink v1.0 9-1/57

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 46027/46083 - 20055A/055BJ
Launch date 07 Aug 2020 - 05:12 UTC
Launch site CCK, LC39A
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

57 satellites launched together (see table).

 Satellite  Cospar nº  Int. Design.  Orbit  Decay
 Starlink v1.0 9-1 (1522)  2020-055A  46027  553.4 x 555.4 x 53.1  
 Starlink v1.0 9-2 (1523)  2020-055B  46028    
 Starlink v1.0 9-3 (1526)  2020-055C  46029    
 Starlink v1.0 9-4 (1534)  2020-055D  46030    
 Starlink v1.0 9-5 (1544)  2020-055E  46031    
 Starlink v1.0 9-6 (1555)  2020-055F  46032    
 Starlink v1.0 9-7 (1556)  2020-055G  46033    
 Starlink v1.0 9-8 (1557)  2020-055H  46034    
 Starlink v1.0 9-9 (1558)  2020-055J  46035    
 Starlink v1.0 9-10 (1560)  2020-055K  46036    
 Starlink v1.0 9-11 (1565)  2020-055L  46037    
 Starlink v1.0 9-12 (1567)  2020-055M  46038    
 Starlink v1.0 9-13 (1569)  2020-055N  46039    
 Starlink v1.0 9-14 (1576)  2020-055P  46040    
 Starlink v1.0 9-15 (1580)  2020-055Q  46041    
 Starlink v1.0 9-16 (1581)  2020-055R  46042    
 Starlink v1.0 9-17 (1582)  2020-055S  46043    
 Starlink v1.0 9-18 (1584)  2020-055T  46044    
 Starlink v1.0 9-19 (1591)  2020-055U  46045    
 Starlink v1.0 9-20 (1514)  2020-055V  46046    
 Starlink v1.0 9-21 (1524)  2020-055W  46047    
 Starlink v1.0 9-22 (1527)  2020-055X  46048    
 Starlink v1.0 9-23 (1530)  2020-055Y  46049    
 Starlink v1.0 9-24 (1535)  2020-055Z  46050    
 Starlink v1.0 9-25 (1540)  2020-055AA  46051    
 Starlink v1.0 9-26 (1541)  2020-055AB  46052    
 Starlink v1.0 9-27 (1543)  2020-055AC  46053    
 Starlink v1.0 9-28 (1548)  2020-055AD  46054    
 Starlink v1.0 9-29 (1554)  2020-055AE  46055    
 Starlink v1.0 9-30 (1561)  2020-055AF  46056    
 Starlink v1.0 9-31 (1562)  2020-055AG  46057    
 Starlink v1.0 9-32 (1564)  2020-055AH  46058    
 Starlink v1.0 9-33 (1570)  2020-055AJ  46059    
 Starlink v1.0 9-34 (1572)  2020-055AK  46060    
 Starlink v1.0 9-35 (1573)  2020-055AL  46061    
 Starlink v1.0 9-36 (1574)  2020-055AM  46062    
 Starlink v1.0 9-37 (1577)  2020-055AN  46063    
 Starlink v1.0 9-38 (1583)  2020-055AP  46064    
 Starlink v1.0 9-39(1515)  2020-055AQ  46065    
 Starlink v1.0 9-40 (1525)  2020-055AR  46066    
 Starlink v1.0 4-41(1529)  2020-055AS  46067    
 Starlink v1.0 9-42 (1532)  2020-055AT  46068    
 Starlink v1.0 9-43 (1533)  2020-055AU  46069    
 Starlink v1.0 9-44 (1536)  2020-055AV  46070    
 Starlink v1.0 9-45 (1538)  2020-055AW  46071    
 Starlink v1.0 9-46 (1539)  2020-055AX  46072    
 Starlink v1.0 9-47 (1542)  2020-055AY  46073    
 Starlink v1.0 9-48 (1549)  2020-055AZ  46074    
 Starlink v1.0 9-49(1551)  2020-055BA  46075    
 Starlink v1.0 9-50 (1552)  2020-055BB  46076    
 Starlink v1.0 9-51 (1559)  2020-055BC  46077    
 Starlink v1.0 9-52 (1563)  2020-055BD  46078    
 Starlink v1.0 9-53 (1566)  2020-055BE  46079    
 Starlink v1.0 9-54 (1568)  2020-055BF  46080    
 Starlink v1.0 9-55 (1571)  2020-055BG  46081    
 Starlink v1.0 9-56 (1578)  2020-055BH  46082    
 Starlink v1.0 9-57 (1579)  2020-055BJ  46083    

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 negenth group of 57 Starlink satellites was launched on Aug 07, 2020 from Kennedy Space Center.

External links:


Ref.: #7(JR782), #228 - update: 12.03.21 Home