STARLINK-31877 (59675)

COSPAR: 2024-084X | Alt Name: Starlink 31877

Image
STARLINK-31877 Satellite Image
Additional Sources
Launch Details

Launch Date

May 6, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59675

International Designator

2024-084X

Epoch

Sun, 19 Jul 2026 20:20:58 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

15.55°

Eccentricity

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Argument of Perigee

284.95°

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-31877

Alternative Name

Starlink 31877

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59675U 24084X   26200.84789412  .00000374  00000+0  23116-4 0  9993
2 59675  43.0042  15.5510 0001103 284.9523  75.1206 15.27564519124588

Source: Celestrak

Summary
The Starlink V2M satellite, designated STARLINK-31877 or Starlink 31877, was launched on May 6, 2024, from Cape Canaveral Air Force Station's LC40 using a Falcon 9 launch vehicle. The spacecraft, manufactured by SPXS and owned by the same entity, has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. It weighs 700 kilograms dry and had a launch mass of 730 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays combined with batteries for power. The satellite is part of the Starlink Group 6-57-22 constellation and serves 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 6-57-22

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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