STARLINK-32019 (60147)

COSPAR: 2024-120N | Alt Name: Starlink 32019

Image

Additional Sources

Launch Details

Launch Date

June 27, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60147

International Designator

2024-120N

Epoch

Sun, 19 Jul 2026 21:53:08 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

64.09°

Eccentricity

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Argument of Perigee

92.84°

Period

93.85 min

Mean Motion

15.34 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot

3D Visualization

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-32019

Alternative Name

Starlink 32019

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 60147U 24120N   26200.91190891  .00000577  00000+0  28208-4 0  9997

2 60147  53.1608  64.0902 0001380  92.8431 267.2729 15.34393482116648

Source: Celestrak

Summary

The Starlink V2M satellite, designated STARLINK-32019 or Starlink 32019, was launched on June 27, 2024, from the Air Force Eastern Test Range (AFETR) at Launch Complex 40 using a Falcon 9 launch vehicle. This communication satellite is part of the Starlink v2 Mini configuration and belongs to SpaceX (SPXS). The spacecraft has dimensions of 0.3 meters in length and 4.1 meters in diameter, with a span of 29 meters due to its solar arrays. It carries a dry mass of 700 kg and was launched with a total mass of 730 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses Argon ion thrusters for propulsion and is powered by solar arrays complemented by batteries. The satellite's shape consists of a box with a pan configuration.

Starlink is a satellite constellation developed by SpaceX with the aim of providing global broadband internet coverage. Thousands of small satellites are deployed in low Earth orbit (LEO), enabling high-speed internet access even in remote areas. However, the rapid increase in satellites raises concerns about space debris and the potential for collisions, which can lead to further debris creation and endanger other spacecraft. Additionally, the sheer number of Starlink satellites can affect astronomical observations by increasing light pollution. Proper deorbiting plans and international coordination are essential to mitigate these challenges and ensure long-term sustainability in space.

Physical Characteristics

Length

0.3

Diameter

4.1

Span

Dry Mass

700

Launch Mass

730

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 10-3-13

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

Ku/Ka/E-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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