STARLINK-30604 (58075)

COSPAR: 2023-160A | Alt Name: Starlink 30604

Image
STARLINK-30604 Satellite Image
Additional Sources
Launch Details

Launch Date

October 18, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58075

International Designator

2023-160A

Epoch

Sun, 19 Jul 2026 20:58:36 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

51.22°

Eccentricity

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Argument of Perigee

271.76°

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-30604

Alternative Name

Starlink 30604

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58075U 23160A   26200.87403682 -.00000533  00000+0 -98660-5 0  9991
2 58075  43.0035  51.2240 0001105 271.7554  88.3171 15.27572975153168

Source: Celestrak

Summary
STARLINK-30604 is a communication satellite designated by NORAD CAT ID 58075 and OBJECT ID 2023-160A. It was launched on October 18, 2023, from the Cape Canaveral Space Force Station (AFETR) using Falcon 9 as the launch vehicle from LC40. The satellite is part of the Starlink Group 6-23-01 and is manufactured by SPXS. It measures 0.3 meters in length, has a diameter of 4.1 meters, and spans 29 meters. Its dry mass is 700 kilograms with a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses Argon ion thrusters for propulsion and solar arrays along with batteries for power supply. The shape of the satellite is described as Box + pan, and it operates under the ownership of SPXS for communication purposes.

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 6-23-01

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

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