STARLINK-31286 (59082)

COSPAR: 2024-041J | Alt Name: Starlink 31286

Image
STARLINK-31286 Satellite Image
Additional Sources
Launch Details

Launch Date

February 29, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59082

International Designator

2024-041J

Epoch

Sun, 19 Jul 2026 07:26:58 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

287.17°

Eccentricity

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Argument of Perigee

252.37°

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-31286

Alternative Name

Starlink 31286

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59082U 24041J   26200.31040318  .00000609  00000+0  31642-4 0  9999
2 59082  43.0025 287.1742 0001319 252.3674 107.7034 15.27574469134486

Source: Celestrak

Summary
STARLINK-31286 is a Starlink v2 Mini satellite (BUS: Starlink V2M) owned by SPXS and launched on February 29, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. The satellite weighs 700 kg dry and 730 kg at launch. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it is powered by solar arrays and batteries and uses Argon ion thrusters for propulsion. Its purpose is communication within the Starlink Group 6-40-09 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 6-40-09

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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