STARLINK-32078 (60338)

COSPAR: 2024-136K | Alt Name: Starlink 32078

Image
STARLINK-32078 Satellite Image
Additional Sources
Launch Details

Launch Date

August 2, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60338

International Designator

2024-136K

Epoch

Mon, 20 Jul 2026 05:05:42 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

180.16°

Eccentricity

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Argument of Perigee

88.05°

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-32078

Alternative Name

Starlink 32078

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60338U 24136K   26201.21230222  .00000409  00000+0  25937-4 0  9993
2 60338  53.1595 180.1639 0001343  88.0482 272.0672 15.30195830109954

Source: Celestrak

Summary
The Starlink V2M satellite, designated as STARLINK-32078 or Starlink 32078, is a communication satellite built by SPXS and launched on August 2, 2024, from LC39A at AFETR using the Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. The satellite weighs 730 kilograms at launch and has a dry mass of 700 kilograms, powered by solar arrays and batteries. Its equipment includes a Ku/Ka/E-band payload and optical inter-satellite link for communication purposes. The propulsion system uses Argon ion thrusters to maintain its orbit.

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 10-6-10

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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