STARLINK-31455 (59309)

COSPAR: 2024-056P | Alt Name: Starlink 31455

Image
STARLINK-31455 Satellite Image
Additional Sources
Launch Details

Launch Date

March 24, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59309

International Designator

2024-056P

Epoch

Mon, 20 Jul 2026 01:08:56 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

200.04°

Eccentricity

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Argument of Perigee

283.08°

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-31455

Alternative Name

Starlink 31455

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59309U 24056P   26201.04788175 -.00000182  00000+0  29002-5 0  9993
2 59309  43.0030 200.0356 0001271 283.0804  76.9906 15.27572561131430

Source: Celestrak

Summary
The STARLINK-31455 satellite, also known as Starlink 31455, is a communication satellite designed under the Starlink v2 Mini configuration by SpaceX (SPXS). Launched on March 24, 2024, from Launch Pad LC39A at AFETR using a Falcon 9 launch vehicle, it has a BUS type of Starlink V2M. The satellite measures approximately 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It is equipped with a Ku/Ka/E-band payload, an optical inter-satellite link, and powered by solar arrays and batteries. The dry mass of the satellite is 700 kg with a launch mass of 730 kg. It utilizes Argon ion thrusters for propulsion.

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 6-42-14

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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