COSMOS 1906 (18713)

COSPAR: 1987-108A | Alt Name: Kosmos-1906
DECAYED

Image
COSMOS 1906 Satellite Image
Additional Sources
Launch Details

Launch Date

December 26, 1987

Launch Site

PLMSC

Launch Pad

LC16/2

Launch Vehicle

Soyuz-U

Orbital Elements

NORAD ID

18713

International Designator

1987-108A

Decay Date

3/13/1988

Basic Satellite Info

Name

COSMOS 1906

Alternative Name

Kosmos-1906

Type

Payload

Status

Decayed

Owner

PRIR

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
COSMOS 1906 (also known as Kosmos-1906) is an Earth Observation satellite launched by the Soviet Union on December 26, 1987, from Plesetsk Cosmodrome using a Soyuz-U launch vehicle. The spacecraft measures 6.5 meters in length and 2.4 meters in diameter with a span of 6.5 meters and has a dry mass of 2,573 kilograms, the same as its launch mass. It was equipped with two deployable solar arrays and batteries for power generation. Designed to operate for approximately 30 days, COSMOS 1906 utilized a Vostok / Zenit Capsule configuration manufactured by TSSKB and featured a Resurs-F2 payload (No. 1L) for film return missions. The satellite was shaped as a sphere with a DCone structure and included an 11D82M maneuver module along with S5.120 propulsion systems.
Physical Characteristics

Length

6.5

Diameter

2.4

Span

6.5

Dry Mass

2573

Launch Mass

2573

Shape

Sphere + DCone

Radar Cross Section

65.92

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Resurs-F2 No. 1L

Purpose

Earth Observation (film return)

Mission

Earth Observation (film return)

Manufacturer

TSSKB

Life Expectancy

30 days

Bus

Resurs-F2

Configuration

Vostok / Zenit Capsule

Motor

11D82M; S5.120 (maneuver module)

Equipment

Unknown

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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