RADUGA 27 (21132)

COSPAR: 1991-014A | Alt Name: Raduga

Image
RADUGA 27 Satellite Image
Additional Sources
Launch Details

Launch Date

February 28, 1991

Launch Pad

LC81/23

Launch Vehicle

Proton-K/DM-2

Orbital Elements

NORAD ID

21132

International Designator

1991-014A

Epoch

Fri, 03 Jul 2026 21:40:55 GMT

Apogee

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Perigee

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Inclination

13.32°

Right Ascension

336.74°

Eccentricity

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Argument of Perigee

319.41°

Period

1435.07 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

RADUGA 27

Alternative Name

Raduga

Type

Payload

Status

Non-operational

Owner

UNKSR

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 21132U 91014A   26184.90342166 -.00000363  00000-0  00000-0 0  9999
2 21132  13.3234 336.7365 0000493 319.4114  62.7286  1.00343610129482

Source: Celestrak

Summary
RADUGA 27, also known as Raduga, is a communication satellite that was launched on February 28, 1991, from the TYMSC launch site using LC81/23 and the Proton-K/DM-2 launch vehicle. With a dry mass of 1800 kg and equipped with two deployable solar arrays and batteries for power generation, it is part of the KAUR-3 configuration under the Raduga bus series manufactured by NPOPM. The satellite's dimensions are a length of 5.5 meters, diameter of 2.5 meters, and span of 9.5 meters. Its equipment includes 3 Delta-1 C-Band transponders and 3 Delta-2 C-Band transponders for communication purposes. The satellite's shape is described as Step Cyl + 2 Pan with a radar cross-section (RCS) of 3.1622, and it was designed to have an operational lifetime of three years.
Physical Characteristics

Length

5.5

Diameter

2.5

Span

9.5

Dry Mass

1800

Launch Mass

1965

Shape

Step Cyl + 2 Pan

Radar Cross Section

3.1622

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Gran' No. 38L

Purpose

Communication

Mission

Communication

Manufacturer

NPOPM

Life Expectancy

3 years

Bus

Raduga

Configuration

KAUR-3

Motor

Unknown

Equipment

3 Delta-1 C-Band transponders, 3 Delta-2 C-Band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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