STARLINK-30300 (57715)

COSPAR: 2023-129T | Alt Name: Starlink 30300

Image
STARLINK-30300 Satellite Image
Additional Sources
Launch Details

Launch Date

August 27, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57715

International Designator

2023-129T

Epoch

Sun, 19 Jul 2026 03:02:32 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

95.66°

Eccentricity

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Argument of Perigee

262.45°

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-30300

Alternative Name

Starlink 30300

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57715U 23129T   26200.12676051 -.00000241  00000+0  77892-6 0  9996
2 57715  43.0015  95.6611 0001253 262.4539  97.6170 15.27566344160785

Source: Celestrak

Summary
The satellite named STARLINK-30300 (OBJECT_ID: 2023-129T) is a Starlink v2 Mini model operated by SpaceX (SPXS). Launched on August 27, 2023, from LC40 at the Cape Canaveral Space Force Station using a Falcon 9 launch vehicle, this communication satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with an overall span of 29 meters. Equipped with a Ku/Ka/E-band payload and optical inter-satellite link for data transmission, it weighs approximately 700 kilograms dry and had a launch mass of 730 kilograms. The satellite is powered by solar arrays and batteries and uses Argon ion thrusters as its propulsion system. Its structure consists of a box with panels, designed primarily for communication purposes within the Starlink Group 6-11-18 constellation.

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 6-11-18

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

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