STARLINK-1626 (46167)

COSPAR: 2020-057BC | Alt Name: Starlink 1626

Image
STARLINK-1626 Satellite Image
Additional Sources
Launch Details

Launch Date

August 18, 2020

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

46167

International Designator

2020-057BC

Epoch

Sat, 04 Jul 2026 02:50:13 GMT

Apogee

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Perigee

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Inclination

53.04°

Right Ascension

80.74°

Eccentricity

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Argument of Perigee

211.06°

Period

91.00 min

Mean Motion

15.82 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-1626

Alternative Name

Starlink 1626

Type

Payload

Status

Partially operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 46167U 20057BC  26185.11820815  .00209663  00000-0  97133-3 0  9998
2 46167  53.0373  80.7380 0003571 211.0622 149.0189 15.82344205324648

Source: Celestrak

Summary
The satellite named STARLINK-1626 (OBJECT_ID: 2020-057BC) is a part of the Starlink constellation manufactured by SPXS and launched on August 18, 2020, from LC40 at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.2 meters in length, 2.8 meters in diameter, and spans up to 9 meters when fully deployed. The satellite's dry mass is 248 kilograms with an overall launch mass of 260 kilograms. Its payload includes a Ku/Ka-band communication system and optical inter-satellite links for data transmission. It utilizes krypton ion thrusters for propulsion, solar arrays for power generation, and batteries as backup energy sources. The mission purpose is to facilitate global 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

0.2

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-L10-40

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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