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IRS-P3
 

IRS-P3

The IRS-P3 satellite was launched from Sriharikota, India, using Polar Satellite Launch Vehicle – PLSV-D3. IRS-P3 was put in a polar, sun-synchronous orbit at an altitude of 817km with equatorial crossing time of 10:30 A.M in the descending node.

IRS - P3 has an X-ray astronomy and two remote sensing payloads, namely Wide Field Sensor (WiFS) and Modular Optoelectronics Scanner (MOS). The mission caters to oceanography applications.

IRS - P3 WiFS is similar to IRS - 1C WiFS but for the inclusion of an additional band in the Middle Infra-red (MIR) region. This sensor is primarily meant for vegetation dynamic studies while MOS is meant for ocean related studies. MOS has helped the ocean application scientists in developing necessary algorithms for extracting ocean parameters such as phytoplankton, yellow substance and suspended sediments in ocean waters.

Orbit

Near Polar, Sun synchronous

Altitude

817km

Inclination

98.69 deg

Local Time

10.30 A.M

Repetivity

24 days

Orbits/cycle

341

Period

101.35 min

Sensors

WiFS, MOS-A, MOS-B,MOS-C

WiFS Sensor Characteristics

Resolution

188 x 188 (B3 & B4)

188 x 246 (B5)

Swath

770 Km

Repeativity

24 days

Spectral Bands

0.62 - 0.68 microns (B3)

0.77 - 0.86 microns (B4)

1.55 – 1.69 microns (B5)

MOS Sensor Characteristics

Sensor

MOS-A

MOS-B

MOS-C

Resolution (m)

1569 x 1395

523 x 523

523 x 644

Swath (km)

195

200

192

Spectral Bands (microns)

0.755-0.768

0.408-1.01

1.5-1.7

Products

Sensor

Resolution(m) of the sensor

& No. of bands

Coverage

km x km

Data Products

Type

Media

Scale of Photo products


WIFS


188
(three)


770x770


Full scenes with SAT


Digital, FCC


1.2 Million


MOS-A


1569x1395
(four)


195x195


Scene based*
(full pass also)


Digital


-


MOS-B


523x523
(thirteen)


200x200


Scene based*
(full pass also)


Digital

-


MOS-C


523x644
(one)


192x192


Scene based*
(full pass also)


Digital

-

 

*One scene above and one scene below are also provided along with the requested scene