STARLINK-32322 (61720)

COSPAR: 2024-196P | Alt Name: Starlink 32322

Image
STARLINK-32322 Satellite Image
Additional Sources
Launch Details

Launch Date

October 30, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61720

International Designator

2024-196P

Epoch

Sun, 19 Jul 2026 20:06:26 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

206.49°

Eccentricity

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Argument of Perigee

83.49°

Period

93.85 min

Mean Motion

15.34 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-32322

Alternative Name

Starlink 32322

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61720U 24196P   26200.83780580  .00000629  00000+0  29763-4 0  9994
2 61720  53.1589 206.4941 0001065  83.4903 276.6221 15.34390596 97405

Source: Celestrak

Summary
The satellite STARLINK-32322, also known as Starlink 32322, is a communication satellite belonging to the Starlink v2 Mini configuration and part of the Starlink Group 10-13-14 payload. It was launched on October 30, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. It weighs 730 kilograms at launch with a dry mass of 700 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it is powered by solar arrays and batteries. The satellite uses Argon ion thrusters for propulsion and was manufactured by SPXS (SpaceX).

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 10-13-14

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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