STARLINK-31657 (59487)

COSPAR: 2024-071D | Alt Name: Starlink 31657

Image
STARLINK-31657 Satellite Image
Additional Sources
Launch Details

Launch Date

April 13, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59487

International Designator

2024-071D

Epoch

Sun, 19 Jul 2026 16:26:24 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

314.22°

Eccentricity

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Argument of Perigee

277.16°

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-31657

Alternative Name

Starlink 31657

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59487U 24071D   26200.68500172 -.00001138  00000+0 -31853-4 0  9994
2 59487  43.0022 314.2168 0001108 277.1646  82.9080 15.27576476128394

Source: Celestrak

Summary
STARLINK-31657 is a Starlink v2 Mini satellite (BUS: Starlink V2M) owned and operated by SPXS (SpaceX). It was launched on April 13, 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 has a span of 29 meters due to its solar arrays or deployable structures. It carries a Ku/Ka/E-band payload along with an optical inter-satellite link, powered by solar arrays and batteries. Equipped with Argon ion thrusters for propulsion, the satellite weighs 700 kilograms dry (730 kilograms at launch) and is designed primarily for communication purposes. Its shape consists of a box structure complemented by a pan design.

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 6-49-04

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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