STARLINK-31423 (59242)

COSPAR: 2024-049M | Alt Name: Starlink 31423

Image
STARLINK-31423 Satellite Image
Additional Sources
Launch Details

Launch Date

March 16, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59242

International Designator

2024-049M

Epoch

Mon, 20 Jul 2026 03:59:00 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

115.63°

Eccentricity

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Argument of Perigee

270.79°

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-31423

Alternative Name

Starlink 31423

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59242U 24049M   26201.16598260  .00001611  00000+0  68038-4 0  9996
2 59242  43.0026 115.6315 0001327 270.7933  89.2766 15.27583542132663

Source: Celestrak

Summary
The satellite STARLINK-31423 (OBJECT_ID: 2024-049M) is a Starlink v2 Mini configuration built by SpaceX (SPXS). It was launched on March 16, 2024, from Launch Complex 39A at Kennedy Space Center using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters, featuring solar arrays and batteries for power generation. It weighs 700 kilograms dry and had a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and optical inter-satellite links, it is designed for communication purposes using Argon ion thrusters as its propulsion system. The satellite's shape is described as "Box + pan."

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 6-44-12

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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