STARLINK-31308 (59153)

COSPAR: 2024-044B | Alt Name: Starlink 31308

Image
STARLINK-31308 Satellite Image
Additional Sources
Launch Details

Launch Date

March 4, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59153

International Designator

2024-044B

Epoch

Sun, 19 Jul 2026 21:05:43 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

33.66°

Eccentricity

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Argument of Perigee

264.46°

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-31308

Alternative Name

Starlink 31308

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59153U 24044B   26200.87897565  .00000327  00000+0  21399-4 0  9991
2 59153  43.0019  33.6572 0001361 264.4595  95.6102 15.27577634134361

Source: Celestrak

Summary
The satellite named STARLINK-31308 (OBJECT_ID: 2024-044B) is a Starlink v2 Mini configuration built by SPXS and launched on March 4, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters. The satellite weighs 730 kilograms at launch with a dry mass of 700 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, it is powered by solar arrays and batteries. Its propulsion system uses Argon ion thrusters to maintain its orbit. The satellite's shape can be described as box-shaped with a pan configuration. It operates in the US and was launched for communication missions under the ownership of SPXS.

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 6-41-02

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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