TIROS 1 (00029)

COSPAR: 1960-002B | Alt Name: TIROS-A

Image
TIROS 1 Satellite Image
Launch Details

Launch Date

April 1, 1960

Launch Pad

LC-17A

Launch Vehicle

Thor Able II

Orbital Elements

NORAD ID

00029

International Designator

1960-002B

Epoch

Sat, 04 Jul 2026 00:36:13 GMT

Apogee

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Perigee

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Inclination

48.38°

Right Ascension

304.63°

Eccentricity

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Argument of Perigee

339.92°

Period

97.38 min

Mean Motion

14.79 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

TIROS 1

Alternative Name

TIROS-A

Type

Payload

Status

Non-operational

Owner

NASA

Country

United States

Constellation

N/A

Related Satellites

Major Events

First successful weather satellite; provided the first television images of Earth from space.

Latest TLEs
1 00029U 60002B   26185.02515657  .00000585  00000-0  10737-3 0  9991
2 00029  48.3788 304.6252 0022242 339.9198  20.0838 14.78796492544626

Source: Celestrak

Summary
TIROS 1 was a weather satellite launched by NASA on April 1, 1960, from Cape Canaveral Air Force Station using a Thor Able II launch vehicle. The spacecraft measured 1.1 meters in diameter and had a dry mass of 122 kilograms. It was equipped with two vidicon TV cameras for capturing Earth cloud cover images. The satellite operated for 78 days, transmitting over 19,000 usable images during its mission. TIROS 1 provided the first successful television images of the Earth from space, revolutionizing weather forecasting and meteorology. The spacecraft's power came from 9,200 solar cells charging nickel-cadmium batteries, and it was spin-stabilized at approximately 8-12 rpm. TIROS 1 played a significant role in establishing the use of satellites for weather observation and monitoring. Its design and technology paved the way for future satellite-based meteorological systems, including those still in operation today.
Physical Characteristics

Length

0.56

Diameter

1.1

Span

1.1

Dry Mass

122

Launch Mass

122

Shape

Cylindrical

Radar Cross Section

0.803

Visual Magnitude

6.1

Color

Silver (aluminum-clad)

Material Composition

Aluminum alloy and stainless steel.

Technical Details

Payload

Two vidicon TV cameras for cloud cover imaging.

Purpose

Meteorology

Mission

Meteorology

Manufacturer

RCA

Life Expectancy

Operated for 78 days, transmitting over 19,000 usable images.

Bus

TIROS

Configuration

Axial

Motor

Solid-fuel thrusters for spin stabilization.

Equipment

Two 1.27-cm-diameter vidicon TV cameras (one wide-angle and one narrow-angle) for capturing Earth cloud cover images.

Power System

Powered by 9,200 solar cells charging nickel-cadmium batteries.

ADCS

Spin-stabilized at approximately 8-12 rpm.

Transmitter Frequency

235 MHz

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