STARLINK-31605 (59348)

COSPAR: 2024-060A | Alt Name: Starlink 31605

Image
STARLINK-31605 Satellite Image
Additional Sources
Launch Details

Launch Date

March 31, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59348

International Designator

2024-060A

Epoch

Sun, 19 Jul 2026 18:05:56 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

223.36°

Eccentricity

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Argument of Perigee

315.76°

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-31605

Alternative Name

Starlink 31605

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59348U 24060A   26200.75412341  .00005407  00000+0  20603-3 0  9997
2 59348  42.9970 223.3647 0000598 315.7558  44.3246 15.27552173130325

Source: Celestrak

Summary
The Starlink-31605 satellite, also known as Starlink 31605, was launched on March 31, 2024, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. It is part of the Starlink v2 Mini configuration and manufactured by SPXS (SpaceX). The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when fully deployed. With a dry mass of 700 kilograms, it carries a Ku/Ka/E-band payload along with an optical inter-satellite link for communication purposes. It is powered by solar arrays and batteries and equipped with Argon ion thrusters as its propulsion system. The satellite's mission is to provide communication services from its stable orbit achieved on March 31, 2024.

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 6-45-01

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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