NOAA 17 (27453)

COSPAR: 2002-032A | Alt Name: NOAA 17

Image
NOAA 17 Satellite Image
Additional Sources
Launch Details

Launch Date

June 24, 2002

Launch Site

AFWTR

Launch Pad

SLC4W

Launch Vehicle

Titan II SLV

Orbital Elements

NORAD ID

27453

International Designator

2002-032A

Epoch

Sat, 04 Jul 2026 04:52:50 GMT

Apogee

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Perigee

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Inclination

98.87°

Right Ascension

151.19°

Eccentricity

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Argument of Perigee

306.36°

Period

100.96 min

Mean Motion

14.26 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

NOAA 17

Alternative Name

NOAA 17

Type

Payload

Status

Non-operational

Owner

NOAA

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 27453U 02032A   26185.20335656  .00000201  00000-0  10273-3 0  9999
2 27453  98.8661 151.1869 0010717 306.3580  53.6609 14.26243898249419

Source: Celestrak

Summary
NOAA 17 is a meteorology satellite operated by NOAA, launched on June 24, 2002, from AFWTR SLC4W using the Titan II SLV launch vehicle. It has dimensions of 4.2 meters in length, 1.9 meters in diameter, and a span of 7 meters. The satellite's dry mass is 1403 kilograms, which is also its launch mass. Equipped with an ATN bus configuration based on the TIROS-N Bus, NOAA 17 carries instruments including AVHRR/3, ATOVS (HIRS/3, AMSU-A, AMSU-B), SEM-2, ARGOS-2 (DCS-2), and S&RSAT. Power is provided by a deployable solar array and batteries, with an expected lifetime of at least 2 years. The satellite's shape is described as box + pan, and it has a radar cross-section of 4.858 square meters. Manufactured by LMEW, NOAA 17 supports meteorological missions using its specified payload.
Physical Characteristics

Length

4.2

Diameter

1.9

Span

7

Dry Mass

1403

Launch Mass

1403

Shape

Box + Pan

Radar Cross Section

4.858

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

NOAA M/S09

Purpose

Meteorology

Mission

Meteorology

Manufacturer

LMEW

Life Expectancy

2 years minimum

Bus

ATN

Configuration

TIROS-N Bus

Motor

Star-37XFP / ISS

Equipment

AVHRR/3, ATOVS (HIRS/3, AMSU-A, AMSU-B), SEM-2, ARGOS-2 (DCS-2), S&RSAT

Power System

Deployable solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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