STARLINK-32084 (60347)

COSPAR: 2024-136U | Alt Name: Starlink 32084

Image
STARLINK-32084 Satellite Image
Additional Sources
Launch Details

Launch Date

August 2, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60347

International Designator

2024-136U

Epoch

Sun, 19 Jul 2026 05:22:42 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

183.95°

Eccentricity

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Argument of Perigee

83.60°

Period

94.01 min

Mean Motion

15.32 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-32084

Alternative Name

Starlink 32084

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60347U 24136U   26200.22410757  .00000488  00000+0  27508-4 0  9999
2 60347  53.1587 183.9497 0001372  83.5968 276.5190 15.31700968109813

Source: Celestrak

Summary
The satellite STARLINK-32084 (OBJECT_ID: 2024-136U) is a Starlink v2 Mini configuration manufactured by SPXS for communication purposes. It was launched on August 2, 2024, from the LC39A launch pad at AFETR using a Falcon 9 launch vehicle. The satellite measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. Its dry mass is 700 kilograms, while its launch mass was 730 kilograms. It is equipped with Ku/Ka/E-band payload equipment, an optical inter-satellite link, solar arrays, batteries, and Argon ion thrusters for propulsion. The satellite's shape consists of a box and 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 10-6-19

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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