STARLINK-31486 (59181)

COSPAR: 2024-045D | Alt Name: Starlink 31486

Image
STARLINK-31486 Satellite Image
Additional Sources
Launch Details

Launch Date

March 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59181

International Designator

2024-045D

Epoch

Sun, 19 Jul 2026 23:55:53 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

62.10°

Eccentricity

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Argument of Perigee

278.15°

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-31486

Alternative Name

Starlink 31486

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59181U 24045D   26200.99714444  .00000128  00000+0  14170-4 0  9998
2 59181  43.0041  62.0953 0001225 278.1474  81.9239 15.27580654133435

Source: Celestrak

Summary
The satellite named STARLINK-31486, also known as Starlink 31486, is a Starlink v2 Mini communication satellite manufactured by SPXS and owned by the same entity. It was launched on March 10, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when fully extended. It weighs 700 kg dry and had an initial launch mass of 730 kg. Equipped with Ku/Ka/E-band payload and optical inter-satellite link equipment, the satellite is powered by solar arrays and batteries and utilizes Argon ion thrusters for its propulsion system. The mission objective is to provide communication services.

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 6-43-04

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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