STARLINK-32514 (61965)

COSPAR: 2024-210G | Alt Name: Starlink 32514

Image
STARLINK-32514 Satellite Image
Additional Sources
Launch Details

Launch Date

November 14, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61965

International Designator

2024-210G

Epoch

Sun, 19 Jul 2026 06:17:43 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

149.73°

Eccentricity

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Argument of Perigee

251.51°

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-32514

Alternative Name

Starlink 32514

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61965U 24210G   26200.26231476  .00006302  00000+0  23832-3 0  9998
2 61965  43.0013 149.7341 0002783 251.5091 108.5459 15.27582384 95115

Source: Celestrak

Summary
The satellite designated as STARLINK-32514 (OBJECT_ID: 2024-210G) is a Starlink v2 Mini configuration built by SpaceX (SPXS). Launched on November 14, 2024, from LC40 at AFETR using the Falcon 9 launch vehicle, this satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It weighs 700 kilograms dry and had a launch mass of 730 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, the satellite is powered by solar arrays and batteries. Its propulsion system consists of Argon ion thrusters, and it serves communication purposes as part of the Starlink Group 6-68-07 mission.

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 6-68-07

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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