STARLINK-32166 (60257)

COSPAR: 2024-131C | Alt Name: Starlink 32166

Image
STARLINK-32166 Satellite Image
Additional Sources
Launch Details

Launch Date

July 27, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60257

International Designator

2024-131C

Epoch

Mon, 20 Jul 2026 06:00:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

156.93°

Eccentricity

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Argument of Perigee

55.04°

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-32166

Alternative Name

Starlink 32166

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60257U 24131C   26201.25004630  .00040015  00000+0  11899-2 0  9991
2 60257  53.1608 156.9318 0001217  55.0378 210.3408 15.34379737  5863

Source: Celestrak

Summary
STARLINK-32166 is a communication satellite with the OBJECT_ID 2024-131C and part of the Starlink v2 Mini configuration by SpaceX (SPXS). It was launched on July 27, 2024, from Launch Complex 39A at Kennedy Space Center aboard a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. It features equipment such as Ku/Ka/E-band payload and an optical inter-satellite link. The spacecraft has a dry mass of 700 kg and a launch mass of 730 kg, powered by solar arrays and batteries. Its propulsion system includes Argon ion thrusters.

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 10-9-03

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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