STARLINK-31258 (58829)

COSPAR: 2024-017D | Alt Name: Starlink 31258

Image
STARLINK-31258 Satellite Image
Additional Sources
Launch Details

Launch Date

January 24, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58829

International Designator

2024-017D

Epoch

Mon, 20 Jul 2026 07:27:31 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

308.13°

Eccentricity

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Argument of Perigee

97.60°

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-31258

Alternative Name

Starlink 31258

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58829U 24017D   26201.31077919  .00001740  00000+0  62619-4 0  9993
2 58829  53.1585 308.1291 0001426  97.6023 262.5142 15.34396262140362

Source: Celestrak

Summary
STARLINK-31258 is a Starlink V2M satellite, configured as Starlink v2 Mini and manufactured by SpaceX (SPXS). Launched on January 24, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has a dry mass of 700 kg and a launch mass of 730 kg. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters. It is equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, powered by solar arrays and batteries. Its propulsion system includes Argon ion thrusters, and its shape consists of a box with a pan configuration. The satellite's primary mission is to provide communication services as part of the Starlink Group 7-11-04 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 7-11-04

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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