STARLINK-32173 (60586)

COSPAR: 2024-150D | Alt Name: Starlink 32173

Image
STARLINK-32173 Satellite Image
Additional Sources
Launch Details

Launch Date

August 20, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60586

International Designator

2024-150D

Epoch

Sun, 19 Jul 2026 23:29:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

49.84°

Eccentricity

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Argument of Perigee

88.08°

Period

93.85 min

Mean Motion

15.34 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-32173

Alternative Name

Starlink 32173

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60586U 24150D   26200.97852234  .00000303  00000+0  20118-4 0  9998
2 60586  53.1599  49.8447 0001285  88.0772 272.0378 15.34391249108338

Source: Celestrak

Summary
The Starlink V2M satellite designated STARLINK-32173 (OBJECT_ID: 2024-150D) was launched on August 20, 2024, from the Cape Canaveral Space Force Station's LC40 pad using a Falcon 9 launch vehicle. It is part of SpaceX's Starlink constellation and has a box-shaped body with solar arrays for power generation and batteries as backup. The satellite measures approximately 0.3 meters in length, has a diameter of 4.1 meters, and spans 29 meters when its components are fully deployed. With a dry mass of 700 kg and launch mass of 730 kg, it is equipped with an Argon ion thruster propulsion system and carries a Ku/Ka/E-band payload along with an optical inter-satellite link for communication purposes. The satellite's primary mission is to provide global internet coverage as part of the Starlink Group 10-5-04 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 10-5-04

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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