AYAME DEB (38683)

COSPAR: 1979-009F | Alt Name: SVM-2B debris

Image

Additional Sources

Launch Details

Launch Date

February 6, 1979

Launch Site

TANSC

Launch Pad

Launch Vehicle

N-1

Orbital Elements

NORAD ID

38683

International Designator

1979-009F

Epoch

Tue, 09 Apr 2024 02:48:58 GMT

Apogee

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Perigee

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Inclination

9.45°

Right Ascension

325.59°

Eccentricity

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Argument of Perigee

98.39°

Period

849.49 min

Mean Motion

1.70 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

AYAME DEB

Alternative Name

SVM-2B debris

Type

Debris

Status

Space Junk

Owner

NASDA

Country

Japan

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 38683U 79009F   24099.11734436 -.00000126  00000-0  00000+0 0  9995

2 38683   9.4515 325.5934 3725626  98.3948 304.4232  1.69513566 85493

Source: Celestrak

Summary

Space debris, also known as space junk, encompasses all non-functional objects orbiting Earth such as defunct satellites, spent rocket stages, and fragments from collisions or disintegrations. Over time, this debris can accumulate and create an increasingly hazardous environment in orbit. Even tiny fragments, traveling at extremely high velocities, can inflict significant damage on operational satellites and spacecraft. If left unmanaged, the density of debris raises the risk of catastrophic collisions and further fragmentation, compounding the problem and threatening the safety and sustainability of space activities.

Physical Characteristics

Length

Diameter

Span

Dry Mass

Launch Mass

Shape

N/A

Radar Cross Section

0.003

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

SVM-2B debris

Purpose

Unknown

Mission

Unknown

Manufacturer

Unknown

Life Expectancy

Unknown

Bus

Unknown

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

Unknown

ADCS

Unknown

Transmitter Frequency

Unknown

Map

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Latitude

Longitude

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