STARLINK-32807 (62845)

COSPAR: 2025-019S | Alt Name: Starlink 32807

Image
STARLINK-32807 Satellite Image
Additional Sources
Launch Details

Launch Date

January 27, 2025

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62845

International Designator

2025-019S

Epoch

Mon, 20 Jul 2026 06:32:09 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

52.78°

Eccentricity

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Argument of Perigee

277.37°

Period

94.27 min

Mean Motion

15.28 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-32807

Alternative Name

Starlink 32807

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62845U 25019S   26201.27232963  .00019223  00000+0  70564-3 0  9998
2 62845  42.9993  52.7829 0001456 277.3675  82.7011 15.27608013 82618

Source: Celestrak

Summary
The satellite named STARLINK-32807 (also known as Starlink 32807) is a part of the Starlink V2M series, owned by SpaceX (SPXS). It was launched on January 27, 2025, from Launch Complex 40 at Cape Canaveral Air Force Station using a Falcon 9 launch vehicle. The satellite has dimensions of approximately 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters, suggesting the presence of deployable structures such as solar panels or antennas. Its dry mass is 700 kilograms while its launch mass was 730 kilograms. The shape is described as "Box + pan," indicating it has a box-like body with additional elements like solar arrays or communication dishes attached to it. It is part of the Starlink Group 12-7-17 payload, aiming to expand SpaceX's satellite internet constellation in low Earth orbit.

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 12-7-17

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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