TIROS-4 (00226)

COSPAR: 1962-002A | Alt Name: TIROS-D

Image
TIROS-4 Satellite Image
Launch Details

Launch Date

February 8, 1962

Launch Pad

LC-17A

Launch Vehicle

Thor-Delta

Orbital Elements

NORAD ID

00226

International Designator

1962-002A

Epoch

Fri, 03 Jul 2026 19:25:22 GMT

Apogee

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Perigee

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Inclination

48.30°

Right Ascension

295.52°

Eccentricity

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Argument of Perigee

320.50°

Period

99.50 min

Mean Motion

14.47 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-4

Alternative Name

TIROS-D

Type

Payload

Status

Non-operational

Owner

NASA Goddard Space Flight Center

Country

United States

Constellation

TIROS

Related Satellites

Major Events

Launched on February 8, 1962; ceased operations on June 30, 1962.

Latest TLEs
1 00226U 62002A   26184.80928800  .00000039  00000-0  56110-4 0  9995
2 00226  48.2968 295.5228 0076256 320.5019  39.0338 14.47191667370853

Source: Celestrak

Summary
The TIROS-4 satellite was a meteorology satellite launched on February 8, 1962, from Cape Canaveral Air Force Station. It had an octahedral shape and measured 1.07 meters in diameter and 0.56 meters in length, weighing 129 kg at launch. The satellite carried two television camera subsystems for cloud cover imaging and three radiometers to measure Earth's radiation. The TIROS-4 was equipped with solid-fuel thrusters for spin rate control and solar cells charging nickel-cadmium batteries. It was operated by NASA Goddard Space Flight Center and ceased operations on June 30, 1962. The satellite was designed and manufactured by RCA Astro Electronics as part of the TIROS (Television Infrared Observation Satellite) series. The TIROS-4 was a significant contribution to meteorological research, providing valuable data on cloud cover and radiation measurements during its operational period. Its mission and performance are notable examples of early space-based observations for weather forecasting and climate studies.
Physical Characteristics

Length

0.56

Diameter

1.07

Span

1.07

Dry Mass

129

Launch Mass

129

Shape

18-sided right prism

Radar Cross Section

0.8251

Visual Magnitude

5

Color

Silver (aluminum-clad)

Material Composition

Aluminum alloy and stainless steel

Technical Details

Payload

Meteorological instruments

Purpose

Meteorology

Mission

Meteorology

Manufacturer

RCA Astro Electronics

Life Expectancy

Operated nominally until June 30, 1962.

Bus

TIROS

Configuration

18-sided right prism

Motor

Solid-fuel thrusters for spin rate control

Equipment

Two independent television camera subsystems for cloud cover imaging; three radiometers (two-channel low-resolution omnidirectional, five-channel scanning, and medium-resolution scanning radiometer) for measuring Earth's radiation.

Power System

Solar cells charging nickel-cadmium batteries

ADCS

Spin-stabilized with magnetic attitude control

Transmitter Frequency

Unknown

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