STARLINK-31792 (60132)

COSPAR: 2024-118V | Alt Name: Starlink 31792

Image
STARLINK-31792 Satellite Image
Additional Sources
Launch Details

Launch Date

June 24, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60132

International Designator

2024-118V

Epoch

Sun, 19 Jul 2026 18:49:34 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

130.77°

Eccentricity

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Argument of Perigee

78.17°

Period

94.10 min

Mean Motion

15.30 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-31792

Alternative Name

Starlink 31792

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60132U 24118V   26200.78442329  .00002384  00000+0  92546-4 0  9993
2 60132  53.1617 130.7677 0001673  78.1747 281.9442 15.30219154115951

Source: Celestrak

Summary
The Starlink-31792 satellite, also known as Starlink 31792, is a communication satellite belonging to SpaceX (SPXS). Launched on June 24, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle, this satellite is part of the Starlink Group 9-2-20 constellation. It has a configuration known as Starlink v2 Mini and measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. The dry mass of the satellite is 700 kilograms, while its launch mass was 730 kilograms. It is equipped with Ku/Ka/E-band payload, an optical inter-satellite link, solar arrays, batteries, and Argon ion thrusters for propulsion. The primary mission of this satellite is communication.

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 9-2-20

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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