STARLINK-31217 (59036)

COSPAR: 2024-038P | Alt Name: Starlink 31217

Image
STARLINK-31217 Satellite Image
Additional Sources
Launch Details

Launch Date

February 25, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59036

International Designator

2024-038P

Epoch

Mon, 20 Jul 2026 10:41:13 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

259.48°

Eccentricity

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Argument of Perigee

269.44°

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-31217

Alternative Name

Starlink 31217

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59036U 24038P   26201.44529536  .00001149  00000+0  51259-4 0  9999
2 59036  43.0012 259.4846 0001413 269.4432  90.6258 15.27591803136249

Source: Celestrak

Summary
STARLINK-31217 is a Starlink v2 Mini satellite (BUS: Starlink V2M) owned and operated by SPXS. Launched on February 25, 2024, from the Air Force Eastern Test Range LC40 using a Falcon 9 launch vehicle, this communication satellite measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. It has a dry mass of 700 kg and a launch mass of 730 kg. The satellite is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, powered by solar arrays and batteries, and uses Argon ion thrusters for propulsion. Its shape is described as box plus pan 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 6-39-14

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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