STARLINK-31511 (59462)

COSPAR: 2024-068H | Alt Name: Starlink 31511

Image
STARLINK-31511 Satellite Image
Additional Sources
Launch Details

Launch Date

April 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59462

International Designator

2024-068H

Epoch

Mon, 20 Jul 2026 04:20:27 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

6.44°

Eccentricity

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Argument of Perigee

267.97°

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-31511

Alternative Name

Starlink 31511

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59462U 24068H   26201.18087131  .00004772  00000+0  18300-3 0  9990
2 59462  43.0037   6.4429 0001317 267.9706  92.0995 15.27550750128786

Source: Celestrak

Summary
STARLINK-31511 is a Starlink V2M satellite configured as Starlink v2 Mini and operated by SPXS (SpaceX). Launched on April 10, 2024, from Cape Canaveral Air Force Station’s LC40 using a Falcon 9 launch vehicle, it has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when deployed. The satellite weighs 730 kilograms at launch with a dry mass of 700 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it utilizes solar arrays and batteries for power generation. Propulsion is provided by Argon ion thrusters. Its primary mission is communication purposes as part of the Starlink Group 6-48-08 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 6-48-08

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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