STARLINK-31393 (59252)

COSPAR: 2024-049X | Alt Name: Starlink 31393

Image
STARLINK-31393 Satellite Image
Additional Sources
Launch Details

Launch Date

March 16, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59252

International Designator

2024-049X

Epoch

Sun, 19 Jul 2026 18:23:42 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

103.08°

Eccentricity

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Argument of Perigee

273.36°

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-31393

Alternative Name

Starlink 31393

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59252U 24049X   26200.76645993  .00000462  00000+0  26302-4 0  9999
2 59252  43.0019 103.0780 0000785 273.3635  86.7127 15.27578210132779

Source: Celestrak

Summary
The STARLINK-31393 satellite, also known as Starlink 31393, is a communication satellite manufactured by SPXS and part of the Starlink Group 6-44-22. It was launched on March 16, 2024, from LC39A at AFETR using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters, with a dry mass of 700 kilograms and a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, it utilizes solar arrays and batteries for power. The satellite is stabilized using Argon ion thrusters and has the configuration of a Starlink v2 Mini.

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 6-44-22

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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