STARLINK-31761 (59615)

COSPAR: 2024-080Q | Alt Name: Starlink 31761

Image
STARLINK-31761 Satellite Image
Additional Sources
Launch Details

Launch Date

April 28, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59615

International Designator

2024-080Q

Epoch

Thu, 07 May 2026 03:53:29 GMT

Apogee

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Perigee

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Inclination

42.98°

Right Ascension

30.73°

Eccentricity

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Argument of Perigee

228.66°

Period

88.82 min

Mean Motion

16.21 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-31761

Alternative Name

Starlink 31761

Type

Payload

Status

Partially operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59615U 24080Q   26127.16214144  .05273590  88185-5  22600-2 0  9999
2 59615  42.9807  30.7317 0019940 228.6603 131.2568 16.21215187113880

Source: Celestrak

Summary
The STARLINK-31761 satellite, also known as Starlink 31761, is a Starlink v2 Mini communication satellite launched by SpaceX on April 28, 2024, from the Air Force Eastern Test Range using Falcon 9 from Launch Complex 40. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when fully deployed. The satellite weighs 730 kilograms at launch with a dry mass of 700 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays combined with batteries for power. Its shape is described as box-like with a pan 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 6-54-15

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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