Starlink v1.0 3-1/60

USA

Int. spacecraft nº:

US spacecraft nº:


Launch data:

Designation 45044/103 - 20006A/BM
Launch date 29 Jan 2020 - 14:06 UTC
Launch site CC, SLC40
Launch vehicle  Falcon-9 v1.2
Mission Communication
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 3-1 (1132)  2020-006A  45044  553.4 x 555.3 x 53.1  
 Starlink v1.0 3-2 (1120)  2020-006B  45045    
 Starlink v1.0 3-3 (1129)  2020-006C  45046    
 Starlink v1.0 3-4 (1131)  2020-006D  45047    
 Starlink v1.0 3-5 (1134)  2020-006E  45048    
 Starlink v1.0 3-6 (1135)  2020-006F  45049    
 Starlink v1.0 3-7 (1140)  2020-006G  45050    
 Starlink v1.0 3-8 (1141)  2020-006H  45051    
 Starlink v1.0 3-9(1148)  2020-006J  45052    
 Starlink v1.0 3-10 (1155)  2020-006K  45053    
 Starlink v1.0 3-11 (1156)  2020-006L  45054    
 Starlink v1.0 3-12 (1157)  2020-006M  45055    22 Oct 2020 (.6)
 Starlink v1.0 3-13 (1158)  2020-006N  45056    05 Dec 2020 (.4)
 Starlink v1.0 3-14 (1159)  2020-006P  45057    
 Starlink v1.0 3-15 (1162)  2020-006Q  45058    
 Starlink v1.0 3-16 (1165)  2020-006R  45059    
 Starlink v1.0 3-17 (1166)  2020-006S  45060    
 Starlink v1.0 3-18 (1169)  2020-006T  45061    
 Starlink v1.0 3-19 (1171)  2020-006U  45062    
 Starlink v1.0 3-20 (1178)  2020-006V  45063    
 Starlink v1.0 3-21 (1133)  2020-006W  45064    
 Starlink v1.0 3-22 (1139)  2020-006X  45065    
 Starlink v1.0 3-23 (1145)  2020-006Y  45066    
 Starlink v1.0 3-24 (1150)  2020-006Z  45067    
 Starlink v1.0 3-25 (1161)  2020-006AA  45068    
 Starlink v1.0 3-26 (1163)  2020-006AB  45069    
 Starlink v1.0 3-27 (1164)  2020-006AC  45070    
 Starlink v1.0 3-28 (1167)  2020-006AD  45071    
 Starlink v1.0 3-29 (1168)  2020-006AE  45072    
 Starlink v1.0 3-30 (1170)  2020-006AF  45073    
 Starlink v1.0 3-31 (1172)  2020-006AG  45074    
 Starlink v1.0 3-32 (1174)  2020-006AH  45075    
 Starlink v1.0 3-33 (1180)  2020-006AJ  45076    
 Starlink v1.0 3-34 (1182)  2020-006AK  45077    
 Starlink v1.0 3-35 (1177)  2020-006AL  45078    
 Starlink v1.0 3-36 (1149)  2020-006AM  45079    
 Starlink v1.0 3-37 (1153)  2020-006AN  45080    
 Starlink v1.0 3-38 (1151)  2020-006AP  45081    
 Starlink v1.0 3-39(1160)  2020-006AQ  45082    
 Starlink v1.0 3-40 (1190)  2020-006AR  45083    
 Starlink v1.0 3-41(1173)  2020-006AS  45084    
 Starlink v1.0 3-42 (1179)  2020-006AT  45085    
 Starlink v1.0 3-43 (1181)  2020-006AU  45086    
 Starlink v1.0 3-44 (1185)  2020-006AV  45087    
 Starlink v1.0 3-45 (1183)  2020-006AW  45088    
 Starlink v1.0 3-46 (1136)  2020-006AX  45089    
 Starlink v1.0 3-47 (1176)  2020-006AY  45090    
 Starlink v1.0 3-48 (1127)  2020-006AZ  45091    
 Starlink v1.0 3-49(1137)  2020-006BA  45092    
 Starlink v1.0 3-50 (1142)  2020-006BB  45093    
 Starlink v1.0 3-51 (1146)  2020-006BC  45094    
 Starlink v1.0 3-52 (1147)  2020-006BD  45095    
 Starlink v1.0 3-53 (1152)  2020-006BE  45096    
 Starlink v1.0 3-54 (1175)  2020-006BF  45097    19 Mar 2021(.2)
 Starlink v1.0 3-55 (1184)  2020-006BG  45098    
 Starlink v1.0 3-56 (1186)  2020-006BH  45099    
 Starlink v1.0 3-57 (1193)  2020-006BJ  45100    
 Starlink v1.0 3-58 (1194)  2020-006BK  45101    
 Starlink v1.0 3-59 (1195)  2020-006BL  45102    
 Starlink v1.0 3-60 (1196)  2020-006BM  45103    

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-satellite 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:

  • SpaceX launched its first batch of 60 Starlink Ku-band internet satellites on May 24, 2019. The Falcon 9 rocket placed the satellites in a 434 x 442 km x 53.0 deg. Each one is about 200-250 kg (the press kit says 227 kg, but this is suspiciously close to the metric equivalent of 500 pounds, so it′s possible they really mean 500+-50 lb = 227 +- 23 kg). The satellites are a flat panel with krypton-propellant electric thrusters and a single deployable solar panel.
  • The second batch of 60 SpaceX Starlink satellites were launched on Nov 11, 2019.
    The Falcon 9 launch vehicle used first stage B1048 on its fourth flight; the stage landed on the OCISLY drone ship and the second stage was deorbited south of Australia, leaving the 60 payloads and four deployment rods in orbit. The new satellites have both Ka and Ku band antennae.
    This time the payloads were deployed in a 298 x 303 km x 53.0 deg orbit; the deployment rods seem to have been ejected in a retrograde direction and are in a 275 x 288 km orbit.

External links:


Ref.: #3(SD576,578,581), #7(JR775), #127, #228 - update: 19.05.21 Home