STARLINK-32154 (60276)

COSPAR: 2024-131X | Alt Name: Starlink 32154

Image
STARLINK-32154 Satellite Image
Additional Sources
Launch Details

Launch Date

July 27, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60276

International Designator

2024-131X

Epoch

Mon, 20 Jul 2026 02:07:23 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

157.15°

Eccentricity

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Argument of Perigee

96.88°

Period

94.11 min

Mean Motion

15.30 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-32154

Alternative Name

Starlink 32154

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60276U 24131X   26201.08846230  .00000628  00000+0  33362-4 0  9990
2 60276  53.1603 157.1523 0001334  96.8847 263.2306 15.30174273111994

Source: Celestrak

Summary
STARLINK-32154 is a Starlink v2 Mini satellite, also known as Starlink 32154, launched on July 27, 2024, from LC39A at AFETR using a Falcon 9 launch vehicle. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters when deployed. It has a dry mass of 700 kilograms and launched with a mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it uses solar arrays and batteries for power. The satellite is owned by SPXS and manufactured by the same entity to provide communication services utilizing Argon ion thrusters for propulsion. Its shape consists of a box design with a pan configuration.

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 10-9-22

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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