STARLINK-31888 (59788)

COSPAR: 2024-093G | Alt Name: Starlink 31888

Image

Additional Sources

Launch Details

Launch Date

May 18, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59788

International Designator

2024-093G

Epoch

Mon, 20 Jul 2026 00:01:53 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

181.43°

Eccentricity

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Argument of Perigee

283.03°

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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-31888

Alternative Name

Starlink 31888

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 59788U 24093G   26201.00131053 -.00000104  00000+0  57534-5 0  9993

2 59788  43.0026 181.4260 0001307 283.0294  77.0411 15.27573113122937

Source: Celestrak

Summary

The Starlink V2M satellite, designated STARLINK-31888 or Starlink 31888, was launched on May 18, 2024, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It carries a Ku/Ka/E-band payload and an optical inter-satellite link, powered by solar arrays and batteries. Its dry mass is 700 kilograms, while its launch mass was 730 kilograms. The satellite uses Argon ion thrusters for propulsion and was manufactured by SpaceX (SPXS) with the purpose of communication as part of the Starlink Group 6-59-07 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

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 6-59-07

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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Latitude

Longitude

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