STARLINK-31795 (59645)

COSPAR: 2024-082Q | Alt Name: Starlink 31795

Image
STARLINK-31795 Satellite Image
Additional Sources
Launch Details

Launch Date

May 3, 2024

Launch Pad

LC101

Launch Vehicle

Chang Zheng 5

Orbital Elements

NORAD ID

59645

International Designator

2024-082Q

Epoch

Sun, 19 Jul 2026 08:02:30 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

57.78°

Eccentricity

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Argument of Perigee

269.77°

Period

94.27 min

Mean Motion

15.28 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-31795

Alternative Name

Starlink 31795

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59645U 24082Q   26200.33507912  .00001106  00000+0  49732-4 0  9991
2 59645  43.0048  57.7781 0001625 269.7680  90.2986 15.27579387125610

Source: Celestrak

Summary
The Starlink V2M satellite, identified by NORAD_CAT_ID 59645 and OBJECT_ID 2024-082Q, was launched on May 3, 2024, from the AFETR launch site using a Chang Zheng 5 rocket. It is part of the Starlink v2 Mini configuration and belongs to SPXS (SpaceX). The satellite measures 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters, weighing 730 kilograms at launch and 700 kilograms dry mass. It is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. The satellite is powered by solar arrays and batteries and uses Argon ion thrusters for propulsion.

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 6-55-15

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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