STARLINK-31201 (58870)

COSPAR: 2024-019T | Alt Name: Starlink 31201

Image
STARLINK-31201 Satellite Image
Additional Sources
Launch Details

Launch Date

January 29, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58870

International Designator

2024-019T

Epoch

Sun, 19 Jul 2026 11:39:53 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

224.21°

Eccentricity

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Argument of Perigee

273.17°

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-31201

Alternative Name

Starlink 31201

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58870U 24019T   26200.48603296 -.00003856  00000+0 -13061-3 0  9999
2 58870  43.0006 224.2057 0001350 273.1719  86.8978 15.27594559139229

Source: Celestrak

Summary
The Starlink V2M satellite, designated as STARLINK-31201 or Starlink 31201, is a communication satellite launched on January 29, 2024, from LC39A at the AFETR launch site using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. The satellite weighs 730 kilograms at launch and has a dry mass of 700 kilograms, equipped with Argon ion thrusters for propulsion and solar arrays along with batteries for power. Its equipment includes Ku/Ka/E-band payload and an optical inter-satellite link. Manufactured by SPXS, the mission is part of the Starlink Group 6-38-18 constellation for communication purposes.

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 6-38-18

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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