STARLINK-31526 (59016)

COSPAR: 2024-036U | Alt Name: Starlink 31526

Image
STARLINK-31526 Satellite Image
Additional Sources
Launch Details

Launch Date

February 23, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59016

International Designator

2024-036U

Epoch

Sun, 19 Jul 2026 02:53:58 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

161.48°

Eccentricity

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Argument of Perigee

143.44°

Period

94.01 min

Mean Motion

15.32 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-31526

Alternative Name

Starlink 31526

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59016U 24036U   26200.12081454 -.00000122  00000+0  78644-5 0  9990
2 59016  53.1596 161.4827 0002106 143.4386 216.6760 15.31699347135813

Source: Celestrak

Summary
The satellite named STARLINK-31526, also known as Starlink 31526, is a communication satellite designed for the Starlink v2 Mini configuration under the ownership of SpaceX (SPXS). Launched on February 23, 2024, from Space Launch Complex 4E at Vandenberg Air Force Base using a Falcon 9 launch vehicle, this satellite has a dry mass of 700 kg and a launch mass of 730 kg. Its dimensions include a length of 0.3 meters, a diameter of 4.1 meters, and a span of 29 meters. The equipment includes a Ku/Ka/E-band payload along with an optical inter-satellite link for communication purposes. It is powered by solar arrays and batteries and uses Argon ion thrusters as its motor system.

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 7-15-19

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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