MIDAS 3 (00163)

COSPAR: 1961-018A | Alt Name: Midas 3

Image
MIDAS 3 Satellite Image
Launch Details

Launch Date

July 12, 1961

Launch Site

Point Arguello

Launch Pad

SLC-3 1-2

Launch Vehicle

Atlas-Agena B

Orbital Elements

NORAD ID

00163

International Designator

1961-018A

Epoch

Sat, 04 Jul 2026 00:32:19 GMT

Apogee

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Perigee

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Inclination

91.12°

Right Ascension

205.96°

Eccentricity

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Argument of Perigee

136.85°

Period

161.46 min

Mean Motion

8.92 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

MIDAS 3

Alternative Name

Midas 3

Type

Payload

Status

Unknown

Owner

Air Force Space Systems Division (AFSSD)

Country

United States

Constellation

MIDAS

Related Satellites

Major Events

First successful launch in the MIDAS program; however, one solar panel failed to deploy, leading to a power failure after five orbits.

Latest TLEs
1 00163U 61018A   26185.02244884 -.00000019  00000-0 -73070-2 0  9991
2 00163  91.1154 205.9613 0102581 136.8519 224.0447  8.91839289115512

Source: Celestrak

Summary
The MIDAS 3 satellite was launched on July 12, 1961, from Point Arguello using an Atlas-Agena B launch vehicle. It was a conical-shaped satellite with a length of 2 meters and a diameter of 1.5 meters, weighing around 840 kg at liftoff. The satellite was designed to detect and track intercontinental ballistic missile (ICBM) launches using its Series III infrared sensor. The MIDAS 3 mission lasted for five orbits before a power failure occurred due to the failure of one solar panel to deploy. Despite this setback, the launch marked the first successful launch in the MIDAS program. The satellite was equipped with two deployable solar arrays and batteries to provide power. It used spin stabilization as its attitude control system. The MIDAS 3 satellite was manufactured by Lockheed Missiles and Space Company (LMSC) for the US Air Force's Space Systems Division (AFSSD). Its primary mission was early warning, designed to detect ICBM launches.
Physical Characteristics

Length

2

Diameter

1.5

Span

2

Dry Mass

840

Launch Mass

1600

Shape

Conical

Radar Cross Section

10.0428

Visual Magnitude

5

Color

Silver

Material Composition

Aluminum and other aerospace materials.

Technical Details

Payload

MIDAS ETS-II F1

Purpose

Early Warning

Mission

Early warning satellite designed to detect intercontinental ballistic missile (ICBM) launches.

Manufacturer

Lockheed Missiles and Space Company (LMSC)

Life Expectancy

The mission lasted for five orbits before a power failure occurred.

Bus

MIDAS

Configuration

Agena-B

Motor

Bell 8081

Equipment

Series III infrared sensor designed to detect and track missile launches.

Power System

Two deployable solar arrays and batteries.

ADCS

Spin stabilization

Transmitter Frequency

Unknown

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