STARLINK-32208 (60598)

COSPAR: 2024-150R | Alt Name: Starlink 32208

Image
STARLINK-32208 Satellite Image
Additional Sources
Launch Details

Launch Date

August 20, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60598

International Designator

2024-150R

Epoch

Sun, 19 Jul 2026 19:19:40 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

53.73°

Eccentricity

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Argument of Perigee

81.01°

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-32208

Alternative Name

Starlink 32208

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60598U 24150R   26200.80533139  .00000176  00000+0  18086-4 0  9992
2 60598  53.1607  53.7327 0001245  81.0117 279.1025 15.30195852108261

Source: Celestrak

Summary
The STARLINK-32208 satellite, also known as Starlink 32208, is a communication satellite designed under the Starlink v2 Mini configuration by SpaceX (SPXS). It was launched on August 20, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. Its dry mass is 700 kg, and it was launched with a total mass of 730 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses Argon ion thrusters for propulsion and solar arrays along with batteries for power generation. It operates in space as part of the Starlink Group 10-5-16 mission to enhance communication services globally.

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 10-5-16

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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