RADUGA-1 7 (28194)

COSPAR: 2004-010A | Alt Name: Raduga-1

Image
RADUGA-1 7 Satellite Image
Additional Sources
Launch Details

Launch Date

March 27, 2004

Launch Pad

LC81/23

Launch Vehicle

Proton-K/DM-2

Orbital Elements

NORAD ID

28194

International Designator

2004-010A

Epoch

Sat, 04 Jul 2026 05:27:17 GMT

Apogee

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Perigee

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Inclination

13.70°

Right Ascension

20.62°

Eccentricity

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Argument of Perigee

234.43°

Period

1436.76 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-1 7

Alternative Name

Raduga-1

Type

Payload

Status

Non-operational

Owner

KVR

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 28194U 04010A   26185.22728404  .00000120  00000-0  00000-0 0  9993
2 28194  13.6968  20.6187 0004189 234.4340 134.7785  1.00225201 81596

Source: Celestrak

Summary
RADUGA-1 7, also known as Raduga-1, is a military communication satellite launched on March 27, 2004, from the TYMCS launch site using LC81/23 and a Proton-K/DM-2 launch vehicle. The satellite has a length of 5 meters, a diameter of 2 meters, and a span of 20 meters with a dry mass of 2200 kg and was launched with a total mass of 2500 kg. It is equipped with 6 Tor C-Band transponders and its power system consists of two deployable solar arrays and batteries. The satellite's design includes a step cylinder shape plus two panels, with an RCS of 12.5893 square meters. RADUGA-1 7 was manufactured by NPOPMR and is owned by KVR, operating under the Globus configuration for military communication purposes, with an expected lifetime of 3 years. The satellite's payload is identified as Globus No. 17L.
Physical Characteristics

Length

5

Diameter

2

Span

20

Dry Mass

2200

Launch Mass

2500

Shape

Step Cyl + 2 Pan

Radar Cross Section

12.5893

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globus No. 17L

Purpose

Military Communication

Mission

Military Communication

Manufacturer

NPOPMR

Life Expectancy

3 years

Bus

Globus

Configuration

KAUR-3

Motor

Unknown

Equipment

6 Tor C-Band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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