STARLINK-31017 (58515)

COSPAR: 2023-191H | Alt Name: Starlink 31017

Image
STARLINK-31017 Satellite Image
Additional Sources
Launch Details

Launch Date

December 7, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58515

International Designator

2023-191H

Epoch

Sun, 19 Jul 2026 17:37:49 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

205.44°

Eccentricity

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Argument of Perigee

280.81°

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-31017

Alternative Name

Starlink 31017

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58515U 23191H   26200.73459882  .00000468  00000+0  26538-4 0  9991
2 58515  43.0030 205.4432 0001365 280.8125  79.2573 15.27575906148370

Source: Celestrak

Summary
The satellite named STARLINK-31017 (OBJECT_ID: 2023-191H) is a Starlink v2 Mini variant manufactured by SPXS and owned by the same entity. It was launched on December 7, 2023, from Cape Canaveral Space Force Station, Launch Complex 40, using a Falcon 9 launch vehicle. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. Its dry mass is 700 kilograms and it had a launch mass of 730 kilograms. It is equipped with Ku/Ka/E-band payload, an optical inter-satellite link, and Argon ion thrusters for propulsion. Power is provided by solar arrays and batteries. The satellite’s primary purpose is communication as part of the Starlink Group 6-33-08 constellation mission.

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 6-33-08

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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