STARLINK-31589 (59654)

COSPAR: 2024-084A | Alt Name: Starlink 31589

Image
STARLINK-31589 Satellite Image
Additional Sources
Launch Details

Launch Date

May 6, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59654

International Designator

2024-084A

Epoch

Sun, 19 Jul 2026 13:32:52 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

16.87°

Eccentricity

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Argument of Perigee

262.04°

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-31589

Alternative Name

Starlink 31589

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59654U 24084A   26200.56449975  .00000419  00000+0  24745-4 0  9995
2 59654  43.0010  16.8700 0001485 262.0436  98.0247 15.27579365124560

Source: Celestrak

Summary
The Starlink-31589 satellite, designated OBJECT_ID 2024-084A and cataloged under NORAD CAT ID 59654, is part of the Starlink v2 Mini configuration manufactured by SpaceX (SPXS). Launched on May 6, 2024, from Launch Complex 40 at Cape Canaveral Air Force Station using a Falcon 9 launch vehicle, this satellite has dimensions including a length of 0.3 meters, a diameter of 4.1 meters, and a span of 29 meters. Equipped with Argon ion thrusters for propulsion and solar arrays along with batteries for power, it carries a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. The satellite has a launch mass of 730 kg and a dry mass of 700 kg.

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 6-57-01

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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