STARLINK-32813 (62869)

COSPAR: 2025-022R | Alt Name: Starlink 32813

Image

Additional Sources

Launch Details

Launch Date

February 1, 2025

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62869

International Designator

2025-022R

Epoch

Sun, 19 Jul 2026 12:56:23 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

236.00°

Eccentricity

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Argument of Perigee

67.80°

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-32813

Alternative Name

Starlink 32813

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 62869U 25022R   26200.53915580  .00007421  00000+0  23056-3 0  9990

2 62869  53.1578 236.0031 0001036  67.7950 292.3162 15.34399113 82106

Source: Celestrak

Summary

The satellite named STARLINK-32813 (also known as Starlink 32813) is a Starlink V2M spacecraft manufactured by SPXS and owned by the same entity, launched on February 1, 2025, from AFWTR. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when deployed. The satellite's dry mass is 700 kilograms, and it had a launch mass of 730 kilograms. Its shape consists of a box with panels for solar power generation. The mission details are not specified, but it belongs to the Starlink Group 11-4-16 payload.

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 11-4-16

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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