STARLINK-32033 (60144)

COSPAR: 2024-120K | Alt Name: Starlink 32033

Image
STARLINK-32033 Satellite Image
Additional Sources
Launch Details

Launch Date

June 27, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60144

International Designator

2024-120K

Epoch

Sun, 19 Jul 2026 19:52:11 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

64.99°

Eccentricity

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Argument of Perigee

87.28°

Period

93.85 min

Mean Motion

15.34 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-32033

Alternative Name

Starlink 32033

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60144U 24120K   26200.82791198  .00000101  00000+0  14128-4 0  9990
2 60144  53.1606  64.9920 0001307  87.2828 272.8324 15.34392271116625

Source: Celestrak

Summary
The satellite identified by NORAD_CAT_ID 60144 and OBJECT_ID 2024-120K is a Starlink V2M spacecraft named STARLINK-32033, or alternatively known as Starlink 32033, manufactured by SPXS (SpaceX). Launched on June 27, 2024, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle, this satellite has a configuration of Starlink v2 Mini. It measures 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. The dry mass is 700 kg, and it carries a Ku/Ka/E-band payload along with an optical inter-satellite link. Equipped with Argon ion thrusters for propulsion and solar arrays combined with batteries for power generation, its primary mission focuses on communication services.

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 10-3-10

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

Map
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