Sputnik 1 (00002)

COSPAR: N/A | Alt Name: Prosteyshiy Sputnik 1 (PS-1)
DECAYED

Image
Sputnik 1 Satellite Image
Launch Details

Launch Date

October 4, 1957

Launch Pad

Site 1/5

Launch Vehicle

Sputnik-PS 8K71PS

Orbital Elements

NORAD ID

00002

International Designator

N/A

Decay Date

1/3/1958

Basic Satellite Info

Name

Sputnik 1

Alternative Name

Prosteyshiy Sputnik 1 (PS-1)

Type

Payload

Status

Decayed

Country

USSR

Constellation

N/A

Related Satellites

Major Events

First artificial Earth satellite; launched on October 4, 1957; transmitted radio signals until October 26, 1957; reentered Earth's atmosphere on January 4, 1958.

Summary
Sputnik 1 was a spherical satellite launched on October 4, 1957, from the Baikonur Cosmodrome by the OKB-1 manufacturer as part of the Sputnik program. The satellite measured 0.58 meters in length and diameter and weighed 83.6 kilograms at launch. It operated for 22 days, transmitting radio signals on frequencies 20.005 MHz and 40.002 MHz until its onboard batteries depleted. The primary objectives of Sputnik 1 were to demonstrate the feasibility of artificial satellites, study the density of the upper atmosphere, and test radio signal propagation through the ionosphere. The satellite's structure consisted of a highly polished silver aluminum-magnesium-titanium alloy with a 1 mm thick heat shield and four external whip antennas. Sputnik 1 reentered Earth's atmosphere on January 4, 1958, after successfully fulfilling its mission objectives. Its launch marked the beginning of the space age, paving the way for subsequent satellite launches, including Sputnik 2 and Sputnik 3, which carried Laika, the first living creature into orbit.
Physical Characteristics

Length

0.58

Diameter

0.58

Span

2.9

Dry Mass

83.6

Launch Mass

83.6

Shape

Spherical with four external whip antennas.

Radar Cross Section

0.018

Visual Magnitude

6

Color

Highly polished silver

Material Composition

Aluminum-magnesium-titanium alloy (AMG6T) with a 1 mm thick heat shield.

Technical Details

Payload

PS-1

Purpose

Scientific research and technology demonstration.

Mission

Demonstrate the feasibility of artificial satellites, study the density of the upper atmosphere, and test radio signal propagation through the ionosphere.

Manufacturer

OKB-1 of NII-88

Life Expectancy

Operated for 22 days, transmitting radio signals until the onboard batteries were depleted on October 26, 1957. The satellite remained in orbit until it reentered Earth's atmosphere on January 4, 1958.

Bus

PS

Configuration

Metal sphere

Motor

N/A

Equipment

Two radio transmitters operating on frequencies 20.005 MHz and 40.002 MHz, four external whip antennas, internal temperature and pressure sensors.

Power System

1 Watt; Powered by three silver-zinc batteries with an expected lifetime of two weeks; the batteries operated for 22 days.

ADCS

N/A

Transmitter Frequency

20.005 MHz, 40.002 MHz

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