STARLINK-31858 (59658)

COSPAR: 2024-084E | Alt Name: Starlink 31858

Image
STARLINK-31858 Satellite Image
Additional Sources
Launch Details

Launch Date

May 6, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59658

International Designator

2024-084E

Epoch

Sun, 19 Jul 2026 19:38:23 GMT

Apogee

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Perigee

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Inclination

43.01°

Right Ascension

15.34°

Eccentricity

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Argument of Perigee

255.94°

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-31858

Alternative Name

Starlink 31858

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59658U 24084E   26200.81833294  .00001849  00000+0  76705-4 0  9999
2 59658  43.0053  15.3358 0001261 255.9384 104.1328 15.27580302124583

Source: Celestrak

Summary
STARLINK-31858 is a Starlink v2 Mini communication satellite (OBJECT_ID: 2024-084E) launched by SpaceX on May 6, 2024, from the Cape Canaveral Space Force Station using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters, featuring solar arrays and batteries for power supply. It weighs 730 kg at launch with a dry mass of 700 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses Argon ion thrusters as its propulsion system. Its mission is to provide communication services as part of the Starlink Group 6-57-05 constellation.

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 6-57-05

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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