EKRAN 14 (15626)

COSPAR: 1985-024A | Alt Name: Ekran

Image
EKRAN 14 Satellite Image
Additional Sources
Launch Details

Launch Date

March 22, 1985

Launch Pad

LC200/40

Launch Vehicle

Proton-K/DM

Orbital Elements

NORAD ID

15626

International Designator

1985-024A

Epoch

Sat, 04 Jul 2026 03:34:01 GMT

Apogee

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Perigee

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Inclination

11.92°

Right Ascension

321.09°

Eccentricity

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Argument of Perigee

1.76°

Period

1519.01 min

Mean Motion

0.95 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 14

Alternative Name

Ekran

Type

Payload

Status

Non-operational

Owner

MSVYAZ

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 15626U 85024A   26185.14862372 -.00000129  00000-0  00000-0 0  9997
2 15626  11.9177 321.0884 0019174   1.7572   2.4316  0.94798384122449

Source: Celestrak

Summary
EKRAN 14, also known as Ekran, is a communication and direct broadcasting satellite operated by MSVYAZ. Launched on March 22, 1985, from the TYSMS launch site using a Proton-K/DM launch vehicle, it has a cylindrical shape with two panels and a plate. The satellite's dimensions are 5.5 meters in length, 2.5 meters in diameter, and spans 9 meters when deployed. It was manufactured by NPOPM and carries the payload Ekran No. 28L, which includes 1 (+1) UHF 200 W transponder with a C-band uplink for communication purposes. The satellite has a launch mass of 2000 kg and a dry mass of 1850 kg. It is powered by two deployable solar arrays and batteries. EKRAN 14's expected lifetime was approximately three years, and it was designed to facilitate direct broadcasting communications from its orbit.
Physical Characteristics

Length

5.5

Diameter

2.5

Span

9

Dry Mass

1850

Launch Mass

2000

Shape

Cyl + 2 Pan + Plate

Radar Cross Section

10.1485

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Ekran No. 28L

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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