EKRAN 7 (12564)

COSPAR: 1981-061A | Alt Name: Ekran

Image
EKRAN 7 Satellite Image
Additional Sources
Launch Details

Launch Date

June 26, 1981

Launch Pad

LC200/40

Launch Vehicle

Proton-K/DM

Orbital Elements

NORAD ID

12564

International Designator

1981-061A

Epoch

Fri, 03 Jul 2026 21:26:26 GMT

Apogee

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Perigee

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Inclination

6.49°

Right Ascension

292.94°

Eccentricity

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Argument of Perigee

63.43°

Period

1436.77 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 7

Alternative Name

Ekran

Type

Payload

Status

Non-operational

Owner

MSVYAZ

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 12564U 81061A   26184.89336589 -.00000200  00000-0  00000-0 0  9999
2 12564   6.4891 292.9392 0004412  63.4312 336.2748  1.00224720129681

Source: Celestrak

Summary
EKRAN 7, also known as Ekran, is a communication and direct broadcasting satellite with the OBJECT_ID of 1981-061A and NORAD_CAT_ID of 12564. It was launched on June 26, 1981, from Tyuratam (TYMSC) Launch Complex 200/40 using a Proton-K/DM launch vehicle. The satellite has a length of 5.5 meters, a diameter of 2.5 meters, and a span of 9 meters, with a dry mass of 1850 kg and a launch mass of 2000 kg. Its configuration is KAUR-3, and it was manufactured by NPOPM for MSVYAZ. The satellite's equipment includes one (+1) UHF 200 W transponder with a C-band uplink and power from two deployable solar arrays and batteries. EKRAN 7 has an RCS of 5.0059, a shape described as cylindrical with two panels and a plate, and was designed to have a lifetime of about three years.
Physical Characteristics

Length

5.5

Diameter

2.5

Span

9

Dry Mass

1850

Launch Mass

2000

Shape

Cyl + 2 Pan + Plate

Radar Cross Section

5.0059

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Ekran No. 21L

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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