ENVISAT (27386)

COSPAR: 2002-009A | Alt Name: Envisat

Image
ENVISAT Satellite Image
Additional Sources
Launch Details

Launch Date

March 1, 2002

Launch Site

FRGUI

Launch Pad

ELA3

Launch Vehicle

Ariane 5G

Orbital Elements

NORAD ID

27386

International Designator

2002-009A

Epoch

Sat, 04 Jul 2026 07:19:49 GMT

Apogee

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Perigee

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Inclination

98.38°

Right Ascension

136.24°

Eccentricity

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Argument of Perigee

85.47°

Period

100.06 min

Mean Motion

14.39 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

ENVISAT

Alternative Name

Envisat

Type

Payload

Status

Non-operational

Owner

ESA

Country

European Space Agency

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 27386U 02009A   26185.30542897  .00000111  00000-0  49888-4 0  9991
2 27386  98.3841 136.2427 0001394  85.4656  86.9277 14.39068879275948

Source: Celestrak

Summary
ENVISAT, also known as Envisat, is an Earth observation satellite with the OBJECT_ID 2002-009A, launched on March 1, 2002, from the ELA3 launch pad at FRGUI using Ariane 5G. It has a configuration of PPF/SPOT Mk.2 and belongs to I-ESA (International-Europe Space Agency). The satellite measures 10 meters in length, 4.5 meters in diameter, with a span of 26 meters. It carries instruments such as MIPAS, GOMOS, SCIAMACHY, MERIS, AATSR, ASAR, RA-2, MWR, DORIS, and LRR for its mission. ENVISAT has a dry mass of 7911 kg and was launched with a total mass of 8211 kg. Its power system consists of deployable solar arrays and batteries. The satellite achieved an operational lifetime of 10 years, surpassing the initial design life of 5 years. Manufactured by ASTD, ENVISAT's shape is described as Box + Pan, with a radar cross-section (RCS) of 18.597 m².
Physical Characteristics

Length

10

Diameter

4.5

Span

26

Dry Mass

7911

Launch Mass

8211

Shape

Box + Pan

Radar Cross Section

18.597

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Envisat PPF

Purpose

Earth observation

Mission

Earth observation

Manufacturer

ASTD

Life Expectancy

5 years (design); 10 years (achieved)

Bus

SPOT/PPF

Configuration

PPF/SPOT Mk.2

Motor

AOCS

Equipment

MIPAS, GOMOS, SCIAMACHY, MERIS, AATSR, ASAR, RA-2, MWR, DORIS, LRR

Power System

Deployable solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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