STARLINK-31797 (59634)

COSPAR: 2024-082D | Alt Name: Starlink 31797

Image
STARLINK-31797 Satellite Image
Additional Sources
Launch Details

Launch Date

May 3, 2024

Launch Pad

LC101

Launch Vehicle

Chang Zheng 5

Orbital Elements

NORAD ID

59634

International Designator

2024-082D

Epoch

Sun, 19 Jul 2026 18:36:28 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

113.78°

Eccentricity

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Argument of Perigee

258.04°

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-31797

Alternative Name

Starlink 31797

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59634U 24082D   26200.77533220 -.00000508  00000+0 -89274-5 0  9991
2 59634  43.0014 113.7795 0000808 258.0419 102.0342 15.27580456125057

Source: Celestrak

Summary
The satellite STARLINK-31797 (OBJECT_ID: 2024-082D) is a Starlink v2 Mini communication satellite manufactured by SPXS and launched on May 3, 2024, from the AFETR launch site using LC101 pad with a Chang Zheng 5 launch vehicle. It has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. The satellite weighs 700 kilograms dry and 730 kilograms at launch. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays with batteries for power. Its mission is to provide communication services as part of the Starlink Group 6-55-04 constellation. The satellite's shape consists of a box with a 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 6-55-04

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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