STARLINK-31165 (58748)

COSPAR: 2024-005W | Alt Name: Starlink 31165

Image
STARLINK-31165 Satellite Image
Additional Sources
Launch Details

Launch Date

January 7, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58748

International Designator

2024-005W

Epoch

Sun, 19 Jul 2026 17:08:19 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

194.28°

Eccentricity

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Argument of Perigee

271.01°

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-31165

Alternative Name

Starlink 31165

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58748U 24005W   26200.71411579  .00001955  00000+0  80578-4 0  9999
2 58748  43.0024 194.2805 0001655 271.0085  89.0577 15.27563761140639

Source: Celestrak

Summary
STARLINK-31165, also known as Starlink 31165, is a communication satellite belonging to the Starlink v2 Mini configuration and part of the Starlink Group 6-35-21 payload. It was launched on January 7, 2024, from Cape Canaveral Air Force Station Launch Complex 40 using a Falcon 9 launch vehicle by SpaceX (SPXS). The satellite measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. It carries a Ku/Ka/E-band payload and an optical inter-satellite link, powered by solar arrays and batteries. Equipped with Argon ion thrusters for propulsion, it weighs 700 kg dry and had a launch mass of 730 kg. The satellite's shape is described as box + pan.

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 6-35-21

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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