STARLINK-31346 (58943)

COSPAR: 2024-027N | Alt Name: Starlink 31346

Image
STARLINK-31346 Satellite Image
Additional Sources
Launch Details

Launch Date

February 10, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58943

International Designator

2024-027N

Epoch

Sun, 19 Jul 2026 20:00:36 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

53.47°

Eccentricity

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Argument of Perigee

76.03°

Period

94.11 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-31346

Alternative Name

Starlink 31346

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58943U 24027N   26200.83375500  .00001376  00000+0  58610-4 0  9995
2 58943  53.1602  53.4658 0001580  76.0332 284.0844 15.30191741137591

Source: Celestrak

Summary
The Starlink-31346 satellite, also known as Starlink 31346, is a communication satellite designed under the Starlink v2 Mini configuration by SPXS (SpaceX). It was launched on February 10, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. Its dry mass is 700 kg, and it was launched with a mass of 730 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite utilizes solar arrays and batteries for power supply and argon ion thrusters as its motor. It operates in a communication mission as part of the Starlink Group 7-13-13 constellation owned by SpaceX.

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 7-13-13

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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