STARLINK-31528 (59010)

COSPAR: 2024-036N | Alt Name: Starlink 31528

Image
STARLINK-31528 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

59010

International Designator

2024-036N

Epoch

Sun, 19 Jul 2026 09:37:03 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

186.71°

Eccentricity

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Argument of Perigee

70.09°

Period

94.11 min

Mean Motion

15.30 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-31528

Alternative Name

Starlink 31528

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59010U 24036N   26200.40073698  .00001810  00000+0  73261-4 0  9999
2 59010  53.1587 186.7116 0001745  70.0852 290.0336 15.30185835135488

Source: Celestrak

Summary
The Starlink-31528 satellite, also known as Starlink 31528, is a communication satellite designed under the Starlink v2 Mini configuration by SpaceX (SPXS). It was launched on February 23, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and a diameter of 4.1 meters with a span of 29 meters. Its dry mass is 700 kg, while its launch mass was 730 kg. It features a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, powered by solar arrays and batteries. The satellite employs Argon ion thrusters as its propulsion system 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 7-15-13

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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