STARLINK-31167 (58744)

COSPAR: 2024-005S | Alt Name: Starlink 31167

Image
STARLINK-31167 Satellite Image
Additional Sources
Launch Details

Launch Date

January 7, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58744

International Designator

2024-005S

Epoch

Sat, 18 Jul 2026 23:39:53 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

52.81°

Eccentricity

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Argument of Perigee

223.70°

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-31167

Alternative Name

Starlink 31167

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58744U 24005S   26199.98603764 -.00002772  00000+0 -91219-4 0  9994
2 58744  43.0035  52.8149 0000968 223.6986 136.3789 15.27586317142282

Source: Celestrak

Summary
The satellite identified by NORAD CAT ID 58744 and OBJECT ID 2024-005S is a Starlink V2M model under the Starlink v2 Mini configuration, owned and operated by SpaceX (SPXS). Launched on January 7, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, this communication satellite has a dry mass of 700 kg and a launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload capabilities along with an optical inter-satellite link for data transmission. The satellite features solar arrays and batteries for power generation and utilizes Argon ion thrusters as its propulsion system. With dimensions including a length of 0.3 meters, diameter of 4.1 meters, and span of 29 meters, the spacecraft is designed in a box with pan configuration to facilitate its mission objectives.

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 6-35-17

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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