STARLINK-31780 (59432)

COSPAR: 2024-065M | Alt Name: Starlink 31780

Image
STARLINK-31780 Satellite Image
Additional Sources
Launch Details

Launch Date

April 7, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59432

International Designator

2024-065M

Epoch

Sun, 19 Jul 2026 21:42:07 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

26.02°

Eccentricity

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Argument of Perigee

101.49°

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-31780

Alternative Name

Starlink 31780

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59432U 24065M   26200.90425677  .00000298  00000+0  19964-4 0  9991
2 59432  53.1612  26.0190 0001284 101.4884 258.6263 15.34394754129191

Source: Celestrak

Summary
The Starlink-31780 satellite, designated 2024-065M under NORAD, is a part of SpaceX's Starlink v2 Mini constellation. Launched on April 7, 2024, from Vandenberg Space Force Base SLC4E using the Falcon 9 launch vehicle, this communication satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a solar panel span of 29 meters. It carries a Ku/Ka/E-band payload along with an optical inter-satellite link, powered by solar arrays and batteries. The dry mass is 700 kilograms while the launch mass was 730 kilograms. Equipped with Argon ion thrusters for maneuvering, it operates under SpaceX's ownership as part of the Starlink Group 8-1-12 mission, aiming to provide communication services.

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 8-1-12

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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