RADUGA 28 (21821)

COSPAR: 1991-087A | Alt Name: Raduga

Image
RADUGA 28 Satellite Image
Additional Sources
Launch Details

Launch Date

December 19, 1991

Launch Pad

LC81/23

Launch Vehicle

Proton-K/DM-2

Orbital Elements

NORAD ID

21821

International Designator

1991-087A

Epoch

Sat, 04 Jul 2026 00:28:09 GMT

Apogee

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Perigee

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Inclination

13.35°

Right Ascension

340.94°

Eccentricity

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Argument of Perigee

184.95°

Period

1434.93 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 28

Alternative Name

Raduga

Type

Payload

Status

Non-operational

Owner

UNKSR

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 21821U 91087A   26185.01955236  .00000042  00000-0  00000-0 0  9998
2 21821  13.3519 340.9355 0004606 184.9544 179.9139  1.00353244126491

Source: Celestrak

Summary
RADUGA 28, also known as Raduga, is a communication satellite with the OBJECT_ID of 1991-087A, belonging to the Raduga bus configuration type KAUR-3 and operated by UNKSR. Launched on December 19, 1991, from TYMSC using LC81/23 launch pad by Proton-K/DM-2 launch vehicle, it has a dry mass of 1800 kg and was manufactured by NPOPM in SU (Soviet Union). The satellite is equipped with 3 Delta-1 C-Band transponders and 3 Delta-2 C-Band transponders for communication purposes. It measures 5.5 meters in length, has a diameter of 2.5 meters, and spans up to 9.5 meters with its deployable solar arrays that also include batteries as part of the power system. The satellite's shape is described as Step Cyl + 2 Pan with an RCS value of 5.0238, indicating its reflectivity characteristics. Its mission was set for a lifetime duration of 3 years and was launched with a mass of 1965 kg.
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

5.0238

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Gran' No. 39L

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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