COSMOS 2466 [GLONASS-M] (37137)

COSPAR: 2010-041A | Alt Name: Kosmos-2464

Image
COSMOS 2466 [GLONASS-M] Satellite Image
Additional Sources
Launch Details

Launch Date

September 2, 2010

Launch Pad

LC81/24

Launch Vehicle

Proton-M/DM-2

Orbital Elements

NORAD ID

37137

International Designator

2010-041A

Epoch

Thu, 02 Jul 2026 13:09:34 GMT

Apogee

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Perigee

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Inclination

63.90°

Right Ascension

189.55°

Eccentricity

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Argument of Perigee

179.01°

Period

675.70 min

Mean Motion

2.13 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

COSMOS 2466 [GLONASS-M]

Alternative Name

Kosmos-2464

Type

Payload

Status

Non-operational

Owner

KVR/IACG

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 37137U 10041A   26183.54831226  .00000081  00000-0  00000+0 0  9996
2 37137  63.8957 189.5527 0017191 179.0060 180.5337  2.13111912123161

Source: Celestrak

Summary
The COSMOS 2466 [GLONASS-M] satellite, also known as Kosmos-2464, is a navigation satellite launched on September 2, 2010, from the TYMSC launch site using the Proton-M/DM-2 launch vehicle. It has a configuration of a 3-Axis stabilized Uragan-M bus and was manufactured by RESH for KVR/IACG. The satellite measures 4 meters in length, with a diameter of 1.5 meters and a span of 7.8 meters when its solar arrays are deployed. At launch, it had a mass of 1450 kg and a dry mass of 1200 kg. It is powered by two deployable solar arrays and batteries, designed for a mission lifetime of seven years. The satellite's shape consists of a cylinder with antennas and two panels. Its purpose is to support navigation services as part of the GLONASS system, using the Uragan-M No. 36L payload.
Physical Characteristics

Length

4

Diameter

1.5

Span

7.8

Dry Mass

1200

Launch Mass

1450

Shape

Cyl + Ant + 2 Pan

Radar Cross Section

4.3792

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Uragan-M No. 36L

Purpose

Navigation

Mission

Navigation

Manufacturer

RESH

Life Expectancy

7 years

Bus

Uragan

Configuration

3-Axis stabilized Uragan-M bus

Motor

?

Equipment

?

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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