Vanguard 2 (00011)

COSPAR: 1959-001A | Alt Name: Vanguard II

Image
Vanguard 2 Satellite Image
Launch Details

Launch Date

February 17, 1959

Launch Pad

LC-18A

Launch Vehicle

Vanguard SLV-4

Orbital Elements

NORAD ID

00011

International Designator

1959-001A

Epoch

Sat, 04 Jul 2026 06:04:05 GMT

Apogee

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Perigee

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Inclination

32.87°

Right Ascension

20.55°

Eccentricity

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Argument of Perigee

154.06°

Period

120.95 min

Mean Motion

11.91 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

Vanguard 2

Alternative Name

Vanguard II

Type

Payload

Status

Unknown

Country

United States

Constellation

N/A

Related Satellites

Major Events

First weather satellite launched; provided data on Earth's cloud cover and atmospheric density.

Latest TLEs
1 00011U 59001A   26185.25284651  .00001694  00000-0  88490-3 0  9994
2 00011  32.8684  20.5518 1444956 154.0557 214.0298 11.90559699537506

Source: Celestrak

Summary
Vanguard 2 was a weather satellite launched on February 17, 1959, from Cape Canaveral Air Force Station in Florida. The satellite measured cloud-cover distribution and provided information on atmospheric density over its 19-day operational period. It had two optical telescopes with photocells for measuring sunlight reflected from Earth's surface. The Vanguard 2 was a small sphere, 10.75 kg (23.6 lbs) in mass and 0.508 meters (1.66 feet) in diameter. Its power source consisted of mercury batteries, and it was equipped with an optical scanner to collect cloud cover data and instruments for measuring atmospheric density. The satellite's spin axis orientation proved unsatisfactory, resulting in poor data quality. The Vanguard 2 mission marked the first launch of a weather satellite into space, providing valuable insights into Earth's cloud cover and atmospheric conditions during its operational period.
Physical Characteristics

Length

0.508

Diameter

0.508

Span

0.508

Dry Mass

10.75

Launch Mass

10.75

Shape

Spherical

Radar Cross Section

0.3823

Visual Magnitude

10.2

Color

Externally covered with an aluminum deposit coated with silicon oxide

Material Composition

Magnesium sphere internally gold-plated and externally covered with an aluminum deposit coated with silicon oxide.

Technical Details

Payload

Optical scanner for cloud cover data and instruments to measure atmospheric density.

Purpose

Science

Mission

Designed to measure cloud-cover distribution over the daylight portion of its orbit and to provide information on the density of the atmosphere.

Manufacturer

Naval Research Laboratory

Life Expectancy

The satellite's optical scanner experiment was designed to operate for 19 days; however, due to an unsatisfactory orientation of the spin axis, the data obtained was poor.

Bus

Vanguard

Configuration

Vanguard 2E

Motor

None

Equipment

Two optical telescopes with photocells for measuring sunlight reflected from Earth's surface and cloud cover.

Power System

Mercury batteries

ADCS

Spin-stabilized at approximately 50 rpm

Transmitter Frequency

108.00 MHz, 108.03 MHz

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