COSMOS 1660 (15821)

COSPAR: 1985-047A | Alt Name: Kosmos-1660

Image
COSMOS 1660 Satellite Image
Additional Sources
Launch Details

Launch Date

June 14, 1985

Launch Site

PLMSC

Launch Pad

LC32/1

Launch Vehicle

Tsiklon-3

Orbital Elements

NORAD ID

15821

International Designator

1985-047A

Epoch

Sat, 04 Jul 2026 05:00:59 GMT

Apogee

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Perigee

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Inclination

73.62°

Right Ascension

162.58°

Eccentricity

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Argument of Perigee

42.21°

Period

116.05 min

Mean Motion

12.41 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

COSMOS 1660

Alternative Name

Kosmos-1660

Type

Payload

Status

Unknown

Owner

NPOPM

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 15821U 85047A   26185.20901689 -.00000021  00000-0 -32077-4 0  9996
2 15821  73.6229 162.5842 0026738  42.2120 329.1287 12.40797868859593

Source: Celestrak

Summary
COSMOS 1660 (also known as Kosmos-1660) is a geodesy satellite manufactured by NPOPM and launched on June 14, 1985, from the PLMSC launch site using a Tsiklon-3 launch vehicle. The spacecraft has dimensions of 5.8 meters in length, 2.4 meters in diameter, and spans 17.8 meters with its deployed solar arrays. It weighs 1556 kilograms at launch and is equipped with Musson No. 17L payload for geodesy purposes. Its power system consists of eight deployable fixed solar arrays and batteries. The satellite has a configuration described as Cyl + 2 Pan + Ant, indicating its cylindrical shape complemented by panels and an antenna. With a surface area (RCS) of 9.8473 square meters, COSMOS 1660 was expected to have a lifespan of 1-2 years following its launch.
Physical Characteristics

Length

5.8

Diameter

2.4

Span

17.8

Dry Mass

1556

Launch Mass

1556

Shape

Cyl + 2 Pan + Ant

Radar Cross Section

9.8473

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Musson No. 17L

Purpose

Geodesy

Mission

Geodesy

Manufacturer

NPOPM

Life Expectancy

1 - 2 years

Bus

KAUR-1 11F666

Configuration

KAUR-1

Motor

Unknown

Equipment

Unknown

Power System

8 deployable fixed solar arrays, solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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