STARLINK-3932 (52576)

COSPAR: 2022-051AS | Alt Name: Starlink 3932

Image
STARLINK-3932 Satellite Image
Additional Sources
Launch Details

Launch Date

May 13, 2022

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

52576

International Designator

2022-051AS

Epoch

Sun, 19 Jul 2026 19:52:01 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

245.64°

Eccentricity

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Argument of Perigee

69.85°

Period

95.44 min

Mean Motion

15.09 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-3932

Alternative Name

Starlink 3932

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 52576U 22051AS  26200.82779014  .00000369  00000+0  41264-4 0  9991
2 52576  53.1589 245.6366 0000956  69.8523 290.2572 15.08828878231539

Source: Celestrak

Summary
STARLINK-3932 is a communication satellite, part of the Starlink Group 4-13-41, manufactured by SPXS and owned by SpaceX (SPXS). Launched on May 13, 2022, from AFWTR's SLC4E launch pad using a Falcon 9 rocket, it has dimensions of 0.2 meters in length, 2.8 meters in diameter, and a span of 9 meters. The satellite carries a Ku/Ka-band payload with an optical inter-satellite link and uses Krypton ion thrusters for propulsion. It is equipped with solar arrays and batteries for power supply and has a dry mass of 275 kg and a launch mass of 297 kg. The purpose of STARLINK-3932 is to provide communication services as part of the Starlink constellation.

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

275

Launch Mass

297

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 4-13-41

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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