STARLINK-32093 (59701)

COSPAR: 2024-086V | Alt Name: Starlink 32093

Image
STARLINK-32093 Satellite Image
Additional Sources
Launch Details

Launch Date

May 8, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59701

International Designator

2024-086V

Epoch

Sun, 19 Jul 2026 14:08:25 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

35.07°

Eccentricity

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Argument of Perigee

252.25°

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-32093

Alternative Name

Starlink 32093

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59701U 24086V   26200.58918382  .00000178  00000+0  15986-4 0  9994
2 59701  43.0030  35.0666 0000864 252.2480 107.8278 15.27577188124282

Source: Celestrak

Summary
The satellite named STARLINK-32093 (OBJECT_ID: 2024-086V) is a Starlink v2 Mini configuration manufactured by SPXS and owned by the same entity. It was launched on May 8, 2024, from Launch Pad LC39A at AFETR using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters. Its dry mass is 700 kg, with an initial launch mass of 730 kg. It features 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's primary purpose is communication as part of the Starlink Group 6-56-20 constellation.

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 6-56-20

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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