STARLINK-31560 (59361)

COSPAR: 2024-060P | Alt Name: Starlink 31560

Image
STARLINK-31560 Satellite Image
Additional Sources
Launch Details

Launch Date

March 31, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59361

International Designator

2024-060P

Epoch

Sun, 19 Jul 2026 18:53:46 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

233.99°

Eccentricity

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Argument of Perigee

283.30°

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-31560

Alternative Name

Starlink 31560

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59361U 24060P   26200.78734279  .00000471  00000+0  26647-4 0  9993
2 59361  42.9996 233.9916 0001217 283.3011  76.7705 15.27576315130263

Source: Celestrak

Summary
The satellite STARLINK-31560 (OBJECT_ID: 2024-060P) is a Starlink V2M spacecraft configured as part of the Starlink v2 Mini series, owned and operated by SPXS in the United States. It was launched on March 31, 2024, from Cape Canaveral Air Force Station's LC40 using a Falcon 9 launch vehicle. The satellite measures 0.3 meters in length, has a diameter of 4.1 meters, and spans 29 meters, featuring solar arrays and batteries for power supply. It weighs 730 kilograms at launch with a dry mass of 700 kilograms. Equipped with Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters, it is designed for communication purposes as part of the Starlink Group 6-45-14 constellation, adopting a box plus pan shape for its structure.

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 6-45-14

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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