STARLINK-1558 (46035)

COSPAR: 2020-055J | Alt Name: Starlink 1558

Image
STARLINK-1558 Satellite Image
Additional Sources
Launch Details

Launch Date

August 7, 2020

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

46035

International Designator

2020-055J

Epoch

Fri, 03 Jul 2026 14:51:42 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

308.18°

Eccentricity

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Argument of Perigee

99.19°

Period

94.01 min

Mean Motion

15.32 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-1558

Alternative Name

Starlink 1558

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 46035U 20055J   26184.61924668 -.00001907  00000-0 -49689-4 0  9992
2 46035  53.1604 308.1801 0001210  99.1863 260.9275 15.31701167326644

Source: Celestrak

Summary
The satellite STARLINK-1558 (OBJECT_ID: 2020-055J) is a Starlink communication satellite manufactured by SpaceX and launched on August 7, 2020, from LC39A at AFETR using the Falcon 9 launch vehicle. The satellite has dimensions of approximately 0.2 meters in length, 2.8 meters in diameter, and spans 9 meters when deployed. It weighs 260 kilograms at launch with a dry mass of 248 kilograms. Equipped with Ku/Ka-band payload (all) and optical inter-satellite links (prototypes), it uses solar arrays and batteries for power generation. The satellite is powered by Krypton ion thrusters and has a box + pan shape, intended for communication purposes as part of the Starlink V1.0-L9-31 constellation 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

0.2

Diameter

2.8

Span

9

Dry Mass

248

Launch Mass

260

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink V1.0-L9-31

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload (all), optical inter-satellite links (a few prototypes)

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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