STARLINK-32350 (61063)

COSPAR: 2024-164P | Alt Name: Starlink 32350

Image
STARLINK-32350 Satellite Image
Additional Sources
Launch Details

Launch Date

September 13, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61063

International Designator

2024-164P

Epoch

Sun, 19 Jul 2026 17:27:12 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

197.07°

Eccentricity

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Argument of Perigee

81.86°

Period

94.01 min

Mean Motion

15.32 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-32350

Alternative Name

Starlink 32350

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61063U 24164P   26200.72722437  .00000774  00000+0  36686-4 0  9997
2 61063  53.1591 197.0736 0001185  81.8562 278.2573 15.31702009103703

Source: Celestrak

Summary
STARLINK-32350 is a communication satellite belonging to the Starlink v2 Mini configuration and operates under the Starlink Group 9-6-14 payload category. It was launched by SpaceX (SPXS) on September 13, 2024, from AFWTR's SLC4E launch pad using a Falcon 9 rocket. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It weighs 730 kilograms at launch and carries a dry mass of 700 kilograms, powered by solar arrays and batteries. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it uses Argon ion thrusters for propulsion and is owned and operated by SpaceX. The satellite's primary purpose is communication, and its shape is described as a box with a 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

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 9-6-14

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

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

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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