STARLINK-30925 (58406)

COSPAR: 2023-180E | Alt Name: Starlink 30925

Image
STARLINK-30925 Satellite Image
Additional Sources
Launch Details

Launch Date

November 22, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58406

International Designator

2023-180E

Epoch

Sun, 19 Jul 2026 21:30:58 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

26.06°

Eccentricity

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Argument of Perigee

267.11°

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-30925

Alternative Name

Starlink 30925

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58406U 23180E   26200.89650961  .00001684  00000+0  70715-4 0  9993
2 58406  43.0033  26.0629 0001345 267.1073  92.9625 15.27579980147729

Source: Celestrak

Summary
STARLINK-30925 is a Starlink V2M satellite, officially designated as 2023-180E and part of the Starlink v2 Mini configuration, launched on November 22, 2023, from Cape Canaveral Air Force Station's LC40 using a Falcon 9 launch vehicle. It measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. The satellite has a dry mass of 700 kg and a launch mass of 730 kg. Its payload includes Ku/Ka/E-band equipment along with an optical inter-satellite link, powered by solar arrays and batteries. The spacecraft is equipped with Argon ion thrusters for propulsion and serves a communication mission operated by SpaceX (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 6-29-05

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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