STARLINK-32407 (62172)

COSPAR: 2024-225K | Alt Name: Starlink 32407

Image
STARLINK-32407 Satellite Image
Additional Sources
Launch Details

Launch Date

November 30, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62172

International Designator

2024-225K

Epoch

Sun, 19 Jul 2026 17:22:52 GMT

Apogee

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Perigee

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Inclination

70.00°

Right Ascension

191.50°

Eccentricity

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Argument of Perigee

264.88°

Period

96.11 min

Mean Motion

14.98 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-32407

Alternative Name

Starlink 32407

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62172U 24225K   26200.72421514  .00002434  00000+0  21171-3 0  9996
2 62172  70.0000 191.4992 0003838 264.8753  95.1968 14.98332345 89657

Source: Celestrak

Summary
STARLINK-32407 is a communication satellite belonging to the Starlink v2 Mini configuration and designated under the Starlink Group N-01-08 payload. Launched on November 30, 2024, from AFWTR's SLC4E launch pad using a Falcon 9 launch vehicle, it was manufactured by SPXS (SpaceX). The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. It weighs 730 kg at launch with a dry mass of 700 kg. Equipped with Ku/Ka/E-band payload and optical inter-satellite link technology, it uses solar arrays and batteries for power generation. Its propulsion system includes Argon ion thrusters. The satellite's shape is described as "Box + pan."

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 N-01-08

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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