STARLINK-31365 (58973)

COSPAR: 2024-031J | Alt Name: Starlink 31365

Image
STARLINK-31365 Satellite Image
Additional Sources
Launch Details

Launch Date

February 15, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58973

International Designator

2024-031J

Epoch

Sun, 19 Jul 2026 20:16:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

42.36°

Eccentricity

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Argument of Perigee

71.86°

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-31365

Alternative Name

Starlink 31365

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58973U 24031J   26200.84449808  .00004434  00000+0  14234-3 0  9998
2 58973  53.1617  42.3560 0001229  71.8592 288.2544 15.34391084136778

Source: Celestrak

Summary
STARLINK-31365 is a communication satellite under the Starlink v2 Mini configuration, launched on February 15, 2024, from SLC4E at AFWTR using a Falcon 9 launch vehicle. It belongs to SPXS and has a BUS type of Starlink V2M. 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 kg, and it was launched at a total mass of 730 kg. It is equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, powered by solar arrays and batteries. The satellite uses Argon ion thrusters as its motor and has a box plus pan shape design.

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 7-14-09

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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