RADUGA-1M 1 (32373)

COSPAR: 2007-058A | Alt Name: Raduga-1M

Image
RADUGA-1M 1 Satellite Image
Additional Sources
Launch Details

Launch Date

December 9, 2007

Launch Pad

LC81/24

Launch Vehicle

Proton-M/Briz-M

Orbital Elements

NORAD ID

32373

International Designator

2007-058A

Epoch

Fri, 03 Jul 2026 18:23:23 GMT

Apogee

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Perigee

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Inclination

10.21°

Right Ascension

51.60°

Eccentricity

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Argument of Perigee

30.33°

Period

1448.75 min

Mean Motion

0.99 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-1M 1

Alternative Name

Raduga-1M

Type

Payload

Status

Non-operational

Owner

KVR

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 32373U 07058A   26184.76624360  .00000089  00000-0  00000-0 0  9990
2 32373  10.2115  51.6049 0001277  30.3275 333.1040  0.99396075 52562

Source: Celestrak

Summary
RADUGA-1M 1, also known as Raduga-1M, is a military communication satellite manufactured by RESH/POLK and owned by KVR. Launched on December 9, 2007, from the TYMSC launch site using a Proton-M/Briz-M launch vehicle, it has a configuration of MSS-2500-GSO and operates with L, C, X, and Ka-band transponders for communication purposes. The satellite measures 5 meters in length, has a diameter of 2 meters, and spans 20 meters when its solar arrays are deployed. It has a dry mass of 2500 kg and launched at 2600 kg with power supplied by two deployable solar arrays and batteries. RADUGA-1M 1 is equipped for a ten-year lifetime and features a step cylindrical shape with two panels, making it identifiable in space due to its radar cross-section (RCS) of 17.9433 square meters.
Physical Characteristics

Length

5

Diameter

2

Span

20

Dry Mass

2500

Launch Mass

2600

Shape

Step Cyl + 2 Pan

Radar Cross Section

17.9433

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globus-1M No. 11L

Purpose

Military Communication

Mission

Military Communication

Manufacturer

RESH/POLK

Life Expectancy

10 years

Bus

Globus

Configuration

MSS-2500-GSO

Motor

Unknown

Equipment

L, C, X and Ka-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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