COSMOS 1703 (16262)

COSPAR: 1985-108A | Alt Name: Kosmos-1703

Image
COSMOS 1703 Satellite Image
Additional Sources
Launch Details

Launch Date

November 22, 1985

Launch Site

PLMSC

Launch Pad

LC32/2

Launch Vehicle

Tsiklon-3

Orbital Elements

NORAD ID

16262

International Designator

1985-108A

Epoch

Sat, 04 Jul 2026 06:55:39 GMT

Apogee

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Perigee

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Inclination

82.45°

Right Ascension

199.03°

Eccentricity

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Argument of Perigee

272.37°

Period

92.55 min

Mean Motion

15.56 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 1703

Alternative Name

Kosmos-1703

Type

Payload

Status

Unknown

Owner

GRU

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 16262U 85108A   26185.28864854  .00035713  00000-0  51325-3 0  9994
2 16262  82.4548 199.0281 0002336 272.3702  87.7284 15.55918275220128

Source: Celestrak

Summary
COSMOS 1703 (also known as Kosmos-1703) is a Tselina-D satellite launched by the Soviet Union on November 22, 1985, from the Plesetsk Cosmodrome using a Tsiklon-3 launch vehicle. The spacecraft has dimensions of 3.2 meters in length and 1.3 meters in diameter with an antenna span of 13.1 meters. It had a dry mass of 1750 kilograms and was launched at the same weight. The satellite's mission is SIGINT (Signal Intelligence) and it was designed for a lifetime of approximately six months. Its power source includes two deployable solar arrays and batteries. COSMOS 1703 was manufactured by YUZH and owned by GRU, with its payload being Ikar No. 44L. The satellite's shape is cylindrical with an antenna structure attached to it, and it has a radar cross-section (RCS) of 7.3663 square meters.
Physical Characteristics

Length

3.2

Diameter

1.3

Span

13.1

Dry Mass

1750

Launch Mass

1750

Shape

Cyl + Ant

Radar Cross Section

7.3663

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Ikar No. 44L

Purpose

SIGINT

Mission

SIGINT

Manufacturer

YUZH

Life Expectancy

6 months

Bus

Tselina-D

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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