STARLINK-32793 (62874)

COSPAR: 2025-022W | Alt Name: Starlink 32793

Image

Additional Sources

Launch Details

Launch Date

February 1, 2025

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62874

International Designator

2025-022W

Epoch

Sun, 19 Jul 2026 11:49:51 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

236.43°

Eccentricity

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Argument of Perigee

48.09°

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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-32793

Alternative Name

Starlink 32793

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 62874U 25022W   26200.49295476  .00010096  00000+0  30952-3 0  9991

2 62874  53.1581 236.4274 0000807  48.0894 312.0177 15.34401886 82098

Source: Celestrak

Summary

The STARLINK-32793 satellite, also known as Starlink 32793, is a part of the Starlink V2M bus series launched by SpaceX (SPXS) on February 1, 2025, from AFWTR launch site. It stabilized in its orbit on February 2, 2025. The satellite has dimensions of approximately 0.3 meters in length and a diameter of 4.1 meters with a span of 29 meters. At launch, it had a mass of 730 kilograms and a dry mass of 700 kilograms. It is categorized under the Starlink Group 11-4-21 payload and is owned by SpaceX. The shape of the satellite is described as "Box + pan."

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

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 11-4-21

Purpose

Unknown

Mission

Unknown

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

Unknown

ADCS

Unknown

Transmitter Frequency

Unknown

Map

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