STARLINK-31697 (59583)

COSPAR: 2024-076V | Alt Name: Starlink 31697

Image
STARLINK-31697 Satellite Image
Additional Sources
Launch Details

Launch Date

April 23, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59583

International Designator

2024-076V

Epoch

Sun, 19 Jul 2026 18:17:30 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

342.92°

Eccentricity

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Argument of Perigee

276.09°

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-31697

Alternative Name

Starlink 31697

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59583U 24076V   26200.76215507 -.00001130  00000+0 -31563-4 0  9990
2 59583  43.0016 342.9205 0000990 276.0868  83.9871 15.27583952126615

Source: Celestrak

Summary
STARLINK-31697, also known as Starlink 31697, is a communication satellite belonging to the Starlink v2 Mini configuration and part of the Starlink Group 6-53-20 payload. Launched on April 23, 2024, from Cape Canaveral Space Force Station's Launch Complex 40 using a Falcon 9 launch vehicle, it has a dry mass of 700 kg and a launch mass of 730 kg. The satellite measures 0.3 meters in length, 4.1 meters in diameter, and its solar arrays span 29 meters. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication, it uses Argon ion thrusters as its motor and is powered by solar arrays and batteries. The satellite was manufactured by SpaceX (SPXS) and is owned by the same entity.

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 6-53-20

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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