COSMOS 1939 (19045)

COSPAR: 1988-032A | Alt Name: Kosmos-1939
DECAYED

Image
COSMOS 1939 Satellite Image
Additional Sources
Launch Details

Launch Date

April 20, 1988

Launch Pad

LC31

Launch Vehicle

Vostok 8A92M

Orbital Elements

NORAD ID

19045

International Designator

1988-032A

Decay Date

10/29/2014

Basic Satellite Info

Name

COSMOS 1939

Alternative Name

Kosmos-1939

Type

Payload

Status

Decayed

Owner

PRIR

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
COSMOS 1939 (Kosmos-1939) is an Earth observation satellite identified by NORAD_CAT_ID as 19045 and OBJECT_ID as 1988-032A. It was launched on April 20, 1988, from the Tyuratam Space Center (TYMSC), Launch Pad LC31, using a Vostok 8A92M launch vehicle. The satellite uses the SP-1 bus and has dimensions of 6.4 meters in length, 1.4 meters in diameter, and a span of 11.6 meters when its solar arrays are deployed. Its dry mass is 1,900 kilograms, which matches its launch mass. COSMOS 1939 is equipped with MSU-E (2), MSU-SK, and MSU-S instruments for Earth observation purposes. It was manufactured by VNIEM under the Resurs-O program and operated by PRIR. The satellite's power system consists of two deployable solar arrays and batteries. Its shape is described as cylindrical with two panels, and it has a radar cross section (RCS) of 5.612 square meters.
Physical Characteristics

Length

6.4

Diameter

1.4

Span

11.6

Dry Mass

1900

Launch Mass

1900

Shape

Cyl + 2 Pan

Radar Cross Section

5.612

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Resurs-O1 No. 2L

Purpose

Earth Observation

Mission

Earth Observation

Manufacturer

VNIEM

Life Expectancy

Unknown

Bus

Resurs-O

Configuration

SP-1 bus

Motor

Unknown

Equipment

MSU-E (2), MSU-SK, MSU-S (#1); MSU-E (2), MSU-SK (#2)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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