STARLINK-31878 (60031)

COSPAR: 2024-111R | Alt Name: Starlink 31878

Image
STARLINK-31878 Satellite Image
Additional Sources
Launch Details

Launch Date

June 8, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60031

International Designator

2024-111R

Epoch

Sun, 19 Jul 2026 19:31:35 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

128.46°

Eccentricity

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Argument of Perigee

80.66°

Period

93.85 min

Mean Motion

15.34 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-31878

Alternative Name

Starlink 31878

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60031U 24111R   26200.81360316 -.00000379  00000+0 -75307-7 0  9996
2 60031  53.1599 128.4555 0001252  80.6600 279.4544 15.34387464119768

Source: Celestrak

Summary
STARLINK-31878 is a Starlink V2M satellite belonging to SpaceX (SPXS) and was launched on June 8, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 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 weighs 730 kg at launch and has a dry mass of 700 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it utilizes solar arrays and batteries for power. The satellite is stabilized by Argon ion thrusters and its mission is to provide communication services as part of the Starlink Group 10-1-16 constellation.

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 10-1-16

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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