STARLINK-11422 [DTC] (61944)

COSPAR: 2024-209F | Alt Name: Starlink 11422

Image
STARLINK-11422 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

November 14, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61944

International Designator

2024-209F

Epoch

Sat, 18 Jul 2026 23:14:36 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

84.33°

Eccentricity

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Argument of Perigee

94.87°

Period

91.73 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
3D Visualization
Basic Satellite Info

Name

STARLINK-11422 [DTC]

Alternative Name

Starlink 11422

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61944U 24209F   26199.96848321  .00136915  00000+0  11148-2 0  9990
2 61944  53.1570  84.3316 0001064  94.8654 265.2486 15.69744422 97293

Source: Celestrak

Summary
The satellite named STARLINK-11422 [DTC], also known as Starlink 11422, is a Starlink V2M model launched on November 14, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. The satellite's dry mass is 700 kg, and it had a launch mass of 730 kg. Manufactured by SPXS, it belongs to the Starlink Group 9-11-06 payload. Its shape consists of a box with a pan configuration. Owned by SpaceX (SPXS), this satellite originates from the United States.

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

29

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 9-11-06

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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