STARLINK-5859 (55915)

COSPAR: 2023-037B | Alt Name: Starlink 5859

Image
STARLINK-5859 Satellite Image
Additional Sources
Launch Details

Launch Date

March 17, 2023

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

55915

International Designator

2023-037B

Epoch

Sun, 19 Jul 2026 19:01:05 GMT

Apogee

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Perigee

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Inclination

70.00°

Right Ascension

331.43°

Eccentricity

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Argument of Perigee

267.60°

Period

96.11 min

Mean Motion

14.98 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-5859

Alternative Name

Starlink 5859

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 55915U 23037B   26200.79241957  .00000047  00000+0  11773-4 0  9997
2 55915  70.0011 331.4290 0003217 267.5959  92.4832 14.98332234183957

Source: Celestrak

Summary
STARLINK-5859 is a communication satellite, part of the Starlink Group 2-8-02, launched by SpaceX (SPXS) on March 17, 2023, from AFWTR Launch Site, SLC4E pad using a Falcon 9 launch vehicle. The satellite has dimensions of 0.2 meters in length and 2.8 meters in diameter with a span of 9 meters. It had a launch mass of 305 kilograms and a dry mass of 290 kilograms. Equipped with a Ku/Ka-band payload, optical inter-satellite link, and Krypton ion thrusters for propulsion, STARLINK-5859 is powered by solar arrays and batteries. Its shape consists of a box with a pan configuration.

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

0.2

Diameter

2.8

Span

9

Dry Mass

290

Launch Mass

305

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 2-8-02

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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