STARLINK-30235 (57294)

COSPAR: 2023-096E | Alt Name: Starlink 30235

Image

Additional Sources

Launch Details

Launch Date

July 10, 2023

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57294

International Designator

2023-096E

Epoch

Sun, 19 Jul 2026 08:28:46 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

199.61°

Eccentricity

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Argument of Perigee

274.64°

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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-30235

Alternative Name

Starlink 30235

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 57294U 23096E   26200.35332079  .00000323  00000+0  21253-4 0  9993

2 57294  43.0008 199.6114 0001225 274.6436  85.4275 15.27577271167758

Source: Celestrak

Summary

The satellite identified by NORAD_CAT_ID 57294 and OBJECT_ID 2023-096E is a Starlink V2M spacecraft designated as STARLINK-30235 or Starlink 30235. It was launched on July 10, 2023, from Cape Canaveral Air Force Station (LC40) using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It carries a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. Its dry mass is 700 kg, while the launch mass was 730 kg. The satellite is powered by solar arrays and batteries and uses Argon ion thrusters for propulsion. The manufacturer of this spacecraft is SPXS (SpaceX), which also owns it. It operates within the Starlink Group 6-5-05 constellation to provide communication services.

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

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 6-5-05

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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