METEOR 3-5 (21655)

COSPAR: 1991-056A | Alt Name: Meteor-3

Image
METEOR 3-5 Satellite Image
Additional Sources
Launch Details

Launch Date

August 15, 1991

Launch Site

PLMSC

Launch Pad

LC32/2

Launch Vehicle

Tsiklon-3

Orbital Elements

NORAD ID

21655

International Designator

1991-056A

Epoch

Sat, 04 Jul 2026 05:03:30 GMT

Apogee

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Perigee

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Inclination

82.56°

Right Ascension

127.34°

Eccentricity

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Argument of Perigee

93.78°

Period

109.33 min

Mean Motion

13.17 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

METEOR 3-5

Alternative Name

Meteor-3

Type

Payload

Status

Unknown

Owner

RGMS

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 21655U 91056A   26185.21076901  .00000184  00000-0  44344-3 0  9993
2 21655  82.5568 127.3439 0014652  93.7814 266.4985 13.17159285676814

Source: Celestrak

Summary
METEOR 3-5, also known as Meteor-3, is a meteorology satellite identified by NORAD_CAT_ID 21655 and OBJECT_ID 1991-056A. It was launched on August 15, 1991, from the Plesetsk Cosmodrome (PLMSC), Launch Pad LC32/2, using a Tsiklon-3 launch vehicle. The satellite operates under SP-2 bus configuration and is owned by RGMS with VNIEM as its manufacturer. It has dimensions of 6.5 meters in length, 2.4 meters in diameter, and a span of 12.7 meters. METEOR 3-5 has a dry mass of 2150 kg and was launched at the same mass. Its power source consists of two deployable solar arrays and batteries. The satellite's shape is described as cylindrical with two panels (Cyl + 2 Pan) and it has an RCS value of 4.7754. It was designed for a mission lifetime of 2 years, primarily focusing on meteorological purposes.
Physical Characteristics

Length

6.5

Diameter

2.4

Span

12.7

Dry Mass

2150

Launch Mass

2150

Shape

Cyl + 2 Pan

Radar Cross Section

4.7754

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Meteor-3 No. 5/TOMS

Purpose

Meteorology

Mission

Meteorology

Manufacturer

VNIEM

Life Expectancy

2 years

Bus

Meteor-3

Configuration

SP-2 bus

Motor

Unknown

Equipment

Unknown

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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