STARLINK-31182 (59159)

COSPAR: 2024-044H | Alt Name: Starlink 31182

Image
STARLINK-31182 Satellite Image
Additional Sources
Launch Details

Launch Date

March 4, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59159

International Designator

2024-044H

Epoch

Sun, 19 Jul 2026 01:50:32 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

84.67°

Eccentricity

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Argument of Perigee

272.10°

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-31182

Alternative Name

Starlink 31182

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59159U 24044H   26200.07676582  .00001424  00000+0  61247-4 0  9998
2 59159  43.0048  84.6735 0001462 272.0993  87.9692 15.27584442133693

Source: Celestrak

Summary
STARLINK-31182 is a communication satellite under the Starlink v2 Mini configuration, operated by SpaceX (SPXS). Launched on March 4, 2024, from LC40 at AFETR 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 up to 29 meters when deployed. It is equipped with Ku/Ka/E-band payload capabilities and an optical inter-satellite link, powered by solar arrays and batteries. Its mission involves providing communication services utilizing Argon ion thrusters for motorization.

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 6-41-08

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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