STARLINK-11326 [DTC] (62010)

COSPAR: 2024-213C | Alt Name: Starlink 11326

Image

Additional Sources

Launch Details

Launch Date

November 18, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62010

International Designator

2024-213C

Epoch

Sun, 19 Jul 2026 23:45:02 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

109.12°

Eccentricity

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Argument of Perigee

58.34°

Period

91.74 min

Mean Motion

15.70 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-11326 [DTC]

Alternative Name

Starlink 11326

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 62010U 24213C   26200.98961794  .00121083  00000+0  98951-3 0  9993

2 62010  53.1571 109.1245 0000968  58.3446 301.7666 15.69716174 95693

Source: Celestrak

Summary

The satellite STARLINK-11326 [DTC], also known as Starlink 11326, is a member of the Starlink V2M series manufactured by SpaceX (SPXS). Launched on November 18, 2024, from Space Launch Complex 4E at AFWTR using a Falcon 9 launch vehicle, it has a dry mass of 700 kg and a launch mass of 730 kg. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters when fully deployed. It is part of the Starlink Group 9-12-03 payload. Its shape is described as "Box + pan," but additional details about its power, purpose, and mission are not provided.

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 9-12-03

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

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