STARLINK-32866 (62858)

COSPAR: 2025-022E | Alt Name: Starlink 32866

Image
STARLINK-32866 Satellite Image
Additional Sources
Launch Details

Launch Date

February 1, 2025

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62858

International Designator

2025-022E

Epoch

Sun, 19 Jul 2026 09:23:53 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

235.08°

Eccentricity

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Argument of Perigee

73.91°

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-32866

Alternative Name

Starlink 32866

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62858U 25022E   26200.39158812  .00001240  00000+0  47847-4 0  9997
2 62858  53.1562 235.0846 0001545  73.9089 286.2084 15.34382659 82109

Source: Celestrak

Summary
The satellite named STARLINK-32866 (OBJECT_ID: 2025-022E) is a Starlink V2M spacecraft manufactured by SPXS and owned by the same entity. It was launched on February 1, 2025, from AFWTR with a launch mass of 730 kg and reached stability on February 2, 2025, at 03:23 UTC. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters. Its dry mass is recorded as 700 kg. The payload it carries is part of the "Starlink Group 11-4-05." The shape of the spacecraft is described as a box with a pan configuration. No additional information regarding its power source, purpose, or major events is provided in the data set.

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 11-4-05

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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