COSMOS 1915 (18809)

COSPAR: 1988-004A | Alt Name: Kosmos-1915
DECAYED

Image
COSMOS 1915 Satellite Image
Additional Sources
Launch Details

Launch Date

January 26, 1988

Launch Site

PLMSC

Launch Pad

LC41/1

Launch Vehicle

Soyuz-U

Orbital Elements

NORAD ID

18809

International Designator

1988-004A

Decay Date

2/9/1988

Basic Satellite Info

Name

COSMOS 1915

Alternative Name

Kosmos-1915

Type

Payload

Status

Decayed

Owner

UNKS

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
COSMOS 1915, also known as Kosmos-1915, is a reconnaissance satellite designed for photo surveillance using film return technology. Launched on January 26, 1988, from the Plesetsk Launch Site (LC41/1) by the Soyuz-U launch vehicle, it was developed and operated under Soviet ownership (SU). The spacecraft has a configuration based on the Zenit bus and is part of the Oblik series. It measures 6 meters in length with a diameter of 2.2 meters and a span of 6 meters. The dry mass is recorded at 2655 kilograms, which is also its launch mass. COSMOS 1915 utilizes batteries for power and has an RCS (Reaction Control System) area of 15.5 square meters. Its shape consists of a sphere combined with a DCone section. The satellite was manufactured by TSSKB and serves the purpose of conducting reconnaissance missions through photographic means that involve film return to Earth.
Physical Characteristics

Length

6

Diameter

2.2

Span

6

Dry Mass

2655

Launch Mass

2655

Shape

Sphere + DCone

Radar Cross Section

15.5

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Oblik No. 363

Purpose

Reconnaissance, photo (film return type)

Mission

Reconnaissance, photo (film return type)

Manufacturer

TSSKB

Life Expectancy

Unknown

Bus

Oblik

Configuration

Zenit bus

Motor

11D82M; S5.120 (maneuver module)

Equipment

Unknown

Power System

Batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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