STARLINK-31466 (59420)

COSPAR: 2024-064Y | Alt Name: Starlink 31466

Image
STARLINK-31466 Satellite Image
Additional Sources
Launch Details

Launch Date

April 5, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59420

International Designator

2024-064Y

Epoch

Mon, 20 Jul 2026 19:54:25 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

24.63°

Eccentricity

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Argument of Perigee

272.41°

Period

94.27 min

Mean Motion

15.28 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-31466

Alternative Name

Starlink 31466

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59420U 24064Y   26201.82946025 -.00000687  00000+0 -15439-4 0  9991
2 59420  43.0049  24.6275 0001077 272.4122  87.6606 15.27569337129589

Source: Celestrak

Summary
STARLINK-31466 is a Starlink v2 Mini satellite operated by SPXS (SpaceX). It was launched on April 5, 2024, from LC40 at AFETR using a 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 and its launch mass was 730 kg. It carries a Ku/Ka/E-band payload, an optical inter-satellite link, and Argon ion thrusters for propulsion. The satellite's power comes from solar arrays and batteries, and it has a box plus panel shape designed for communication purposes.

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 6-47-23

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

Map
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