STARLINK-31439 (59178)

COSPAR: 2024-045A | Alt Name: Starlink 31439

Image
STARLINK-31439 Satellite Image
Additional Sources
Launch Details

Launch Date

March 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59178

International Designator

2024-045A

Epoch

Sun, 19 Jul 2026 23:50:20 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

62.07°

Eccentricity

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Argument of Perigee

275.18°

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-31439

Alternative Name

Starlink 31439

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59178U 24045A   26200.99329079  .00001561  00000+0  66228-4 0  9993
2 59178  43.0020  62.0679 0001013 275.1766  84.8970 15.27581817 69769

Source: Celestrak

Summary
The Starlink V2M satellite, designated as STARLINK-31439 or Starlink 31439, was launched on March 10, 2024, from the Cape Canaveral Space Force Station using a Falcon 9 launch vehicle. The spacecraft is part of the Starlink v2 Mini configuration and is owned by SpaceX (SPXS). It measures 0.3 meters in length with a diameter of 4.1 meters and has a span of 29 meters, equipped with solar arrays and batteries for power supply. Its dry mass is 700 kg while its launch mass was 730 kg. The satellite carries a Ku/Ka/E-band payload along with an optical inter-satellite link and uses Argon ion thrusters as propulsion. It was stabilized by March 11, 2024, and its primary mission is to provide communication services.

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 6-43-01

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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