STARLINK-32585 (61953)

COSPAR: 2024-209Q | Alt Name: Starlink 32585

Image
STARLINK-32585 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

61953

International Designator

2024-209Q

Epoch

Sun, 19 Jul 2026 19:34:22 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

241.03°

Eccentricity

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Argument of Perigee

67.33°

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
3D Visualization
Basic Satellite Info

Name

STARLINK-32585

Alternative Name

Starlink 32585

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61953U 24209Q   26200.81553998  .00009072  00000+0  27928-3 0  9997
2 61953  53.1568 241.0267 0000604  67.3291 292.7776 15.34401577 95230

Source: Celestrak

Summary
STARLINK-32585, also known as Starlink 32585, is a satellite belonging to the Starlink V2M bus series launched by SpaceX on November 14, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. It has dimensions of approximately 0.3 meters in length, 4.1 meters in diameter, and spans about 29 meters when fully deployed. The satellite's dry mass is 700 kilograms with a total launch mass of 730 kilograms. Its shape resembles a box with an added pan configuration. The satellite is part of the Starlink Group 9-11-15 payload and is owned by SpaceX, which also manufactured it.

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 9-11-15

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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