STARLINK-1832 (46780)

COSPAR: 2020-074AT | Alt Name: Starlink 1832

Image
STARLINK-1832 Satellite Image
Additional Sources
Launch Details

Launch Date

October 24, 2020

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

46780

International Designator

2020-074AT

Epoch

Sat, 02 May 2026 01:30:25 GMT

Apogee

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Perigee

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Inclination

53.02°

Right Ascension

354.93°

Eccentricity

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Argument of Perigee

256.77°

Period

87.82 min

Mean Motion

16.40 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-1832

Alternative Name

Starlink 1832

Type

Payload

Status

Partially operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 46780U 20074AT  26122.06279451  .08857773  12320-4  65286-3 0  9992
2 46780  53.0192 354.9333 0009436 256.7748 103.2246 16.39739041305939

Source: Celestrak

Summary
The STARLINK-1832 satellite, also known as Starlink 1832, is a communication spacecraft operated by SpaceX (SPXS). Launched on October 24, 2020, from the Cape Canaveral Space Force Station's LC40 using a Falcon 9 launch vehicle, it is part of the Starlink constellation. With dimensions of 0.2 meters in length and 2.8 meters in diameter, it features a box plus pan shape. The satellite has a dry mass of 248 kilograms and a launch mass of 260 kilograms. Equipped with Ku/Ka-band payload (all), optical inter-satellite links (prototypes), and krypton ion thrusters for propulsion, STARLINK-1832 uses solar arrays and batteries for power supply. The mission aims to provide 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

0.2

Diameter

2.8

Span

9

Dry Mass

248

Launch Mass

260

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink V1.0-L14-02

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload (all), optical inter-satellite links (a few prototypes)

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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