STARLINK-31380 (58979)

COSPAR: 2024-031Q | Alt Name: Starlink 31380

Image
STARLINK-31380 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

58979

International Designator

2024-031Q

Epoch

Sun, 19 Jul 2026 17:11:30 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

42.98°

Eccentricity

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Argument of Perigee

81.27°

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-31380

Alternative Name

Starlink 31380

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58979U 24031Q   26200.71632506 -.00004512  00000+0 -12252-3 0  9996
2 58979  53.1593  42.9765 0001253  81.2667 278.8477 15.34386787136735

Source: Celestrak

Summary
The STARLINK-31380 (OBJECT_ID: 2024-031Q) is a Starlink v2 Mini communication satellite manufactured by SpaceX and launched on February 15, 2024, from the AFWTR launch site using a Falcon 9 rocket. 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 kg at launch and 700 kg dry mass. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it is powered by solar arrays and batteries, featuring Argon ion thrusters for propulsion. Its shape consists of a box with a panel configuration.

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 7-14-15

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

Map
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