STARLINK-30146 (57442)

COSPAR: 2023-105N | Alt Name: Starlink 30146

Image
STARLINK-30146 Satellite Image
Additional Sources
Launch Details

Launch Date

July 24, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57442

International Designator

2023-105N

Epoch

Sun, 19 Jul 2026 19:01:10 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

233.94°

Eccentricity

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Argument of Perigee

276.34°

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-30146

Alternative Name

Starlink 30146

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57442U 23105N   26200.79248514  .00002633  00000+0  10523-3 0  9990
2 57442  43.0000 233.9395 0001221 276.3351  83.7361 15.27557906165847

Source: Celestrak

Summary
The Starlink V2M satellite, identified by NORAD CAT ID 57442 and OBJECT ID 2023-105N, was launched on July 24, 2023, from Launch Pad LC40 at AFETR using a Falcon 9 launch vehicle. It is part of the Starlink v2 Mini configuration and has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters. The satellite's dry mass is 700 kilograms with a total launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays and batteries for power generation. Manufactured by SPXS, its primary mission is communication. The satellite's shape consists of a box 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 6-6-13

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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