STARLINK-32499 (61959)

COSPAR: 2024-210A | Alt Name: Starlink 32499

Image
STARLINK-32499 Satellite Image
Additional Sources
Launch Details

Launch Date

November 14, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61959

International Designator

2024-210A

Epoch

Mon, 20 Jul 2026 05:19:05 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

150.95°

Eccentricity

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Argument of Perigee

267.10°

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-32499

Alternative Name

Starlink 32499

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61959U 24210A   26201.22158840  .00008092  00000+0  30324-3 0  9993
2 61959  42.9996 150.9535 0000882 267.1017  92.9733 15.27582649 95197

Source: Celestrak

Summary
The Starlink V2M satellite, designated as STARLINK-32499 or Starlink 32499, is a communication satellite built by SPXS and launched on November 14, 2024, from the AFETR launch site using Falcon 9 at LC40. It measures 0.3 meters in length, has a diameter of 4.1 meters, and a span of 29 meters. The satellite carries a Ku/Ka/E-band payload with an optical inter-satellite link for communication purposes and is equipped with Argon ion thrusters for propulsion. Its dry mass is 700 kg while the launch mass was 730 kg. Power is supplied by solar arrays and batteries, and it operates in a Box + pan configuration shape.

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 6-68-01

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

Map
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