STARLINK-31019 (58540)

COSPAR: 2023-192K | Alt Name: Starlink 31019

Image
STARLINK-31019 Satellite Image
Additional Sources
Launch Details

Launch Date

December 8, 2023

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58540

International Designator

2023-192K

Epoch

Mon, 20 Jul 2026 04:47:14 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

165.09°

Eccentricity

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Argument of Perigee

88.72°

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
Basic Satellite Info

Name

STARLINK-31019

Alternative Name

Starlink 31019

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58540U 23192K   26201.19947529  .00000016  00000+0  11629-4 0  9995
2 58540  53.1575 165.0908 0001489  88.7182 271.3991 15.34396518146306

Source: Celestrak

Summary
The satellite named STARLINK-31019 (OBJECT_ID: 2023-192K) is a Starlink V2M model configured as Starlink v2 Mini, manufactured by SPXS for communication purposes. It was launched on December 8, 2023, from AFWTR at SLC4E using the Falcon 9 launch vehicle. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. Its dry mass is 700 kg while its launch mass was 730 kg, powered by solar arrays and batteries. It is equipped with a Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters for propulsion. 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

29

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 7-8-10

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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