STARLINK-32202 (60595)

COSPAR: 2024-150N | Alt Name: Starlink 32202

Image
STARLINK-32202 Satellite Image
Additional Sources
Launch Details

Launch Date

August 20, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60595

International Designator

2024-150N

Epoch

Sun, 19 Jul 2026 20:58:01 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

52.74°

Eccentricity

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Argument of Perigee

84.82°

Period

94.01 min

Mean Motion

15.32 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-32202

Alternative Name

Starlink 32202

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60595U 24150N   26200.87362294  .00001414  00000+0  57330-4 0  9999
2 60595  53.1599  52.7427 0001266  84.8193 275.2953 15.31703634108289

Source: Celestrak

Summary
The satellite STARLINK-32202 (OBJECT_ID: 2024-150N) is a Starlink V2M configuration designed for communication purposes. Launched on August 20, 2024, from the AFETR site at LC40 using a Falcon 9 launch vehicle, it belongs to SpaceX and operates as part of the Starlink Group 10-5-13 payload constellation. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. It carries a Ku/Ka/E-band payload with an optical inter-satellite link for communication and is equipped with Argon ion thrusters as motors. Solar arrays and batteries provide power to the satellite, which has a dry mass of 700 kilograms and a launch mass of 730 kilograms.

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 10-5-13

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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