EKRAN 4 (11561)

COSPAR: 1979-087A | Alt Name: Ekran

Image
EKRAN 4 Satellite Image
Additional Sources
Launch Details

Launch Date

October 3, 1979

Launch Pad

LC200/40

Launch Vehicle

Proton-K/DM

Orbital Elements

NORAD ID

11561

International Designator

1979-087A

Epoch

Fri, 03 Jul 2026 20:31:32 GMT

Apogee

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Perigee

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Inclination

5.55°

Right Ascension

284.60°

Eccentricity

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Argument of Perigee

189.22°

Period

1436.29 min

Mean Motion

1.00 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

EKRAN 4

Alternative Name

Ekran

Type

Payload

Status

Non-operational

Owner

MSVYAZ

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 11561U 79087A   26184.85523216 -.00000263  00000-0  00000-0 0  9990
2 11561   5.5527 284.6016 0011261 189.2172 212.2196  1.00258510 47543

Source: Celestrak

Summary
EKRAN 4, also known as Ekran, is a communication and direct broadcasting satellite that was launched on October 3, 1979, from the TYMSC launch site using the Proton-K/DM launch vehicle. With a dry mass of 1850 kg and an initial launch mass of 2000 kg, it has dimensions of 5.5 meters in length and 2.5 meters in diameter, with a span of 9 meters. It was equipped with one UHF 200 W transponder and a C-band uplink for communication purposes. The satellite's power system consists of two deployable solar arrays and batteries. EKRAN 4 had a mission lifetime of approximately three years and was manufactured by NPOPM, owned by MSVYAZ, and its payload was designated as Ekran No. 17L.
Physical Characteristics

Length

5.5

Diameter

2.5

Span

9

Dry Mass

1850

Launch Mass

2000

Shape

Cyl + 2 Pan + Plate

Radar Cross Section

0.1995

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Ekran No. 17L

Purpose

Communication, direct broadcasting

Mission

Communication, direct broadcasting

Manufacturer

NPOPM

Life Expectancy

3 years

Bus

Ekran

Configuration

KAUR-3

Motor

Unknown

Equipment

1 (+1) UHF 200 W transponder, C-band uplink

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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