IRS-P2 (23323)

COSPAR: 1994-068A | Alt Name: IRS-P2

Image
IRS-P2 Satellite Image
Additional Sources
Launch Details

Launch Date

October 15, 1994

Launch Site

SRILR

Launch Pad

FLP

Launch Vehicle

PSLV

Orbital Elements

NORAD ID

23323

International Designator

1994-068A

Epoch

Sat, 04 Jul 2026 01:21:12 GMT

Apogee

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Perigee

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Inclination

98.89°

Right Ascension

235.81°

Eccentricity

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Argument of Perigee

92.95°

Period

101.08 min

Mean Motion

14.25 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

IRS-P2

Alternative Name

IRS-P2

Type

Payload

Status

Non-operational

Owner

ISRO

Country

India

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 23323U 94068A   26185.05639665  .00000106  00000-0  65454-4 0  9997
2 23323  98.8927 235.8079 0001225  92.9465 267.1854 14.24672136647463

Source: Celestrak

Summary
IRS-P2 is an Earth observation satellite with NORAD identification number 23323 and OBJECT_ID 1994-068A. It was launched on October 15, 1994, from the Sriharikota Launch Pad (FLP) using a PSLV launch vehicle. The satellite operates under the IRS-1 Bus configuration with a length of 1.6 meters and a diameter of 1.1 meters, featuring a box shape with two panoramic sections and a span of 12 meters. Equipped with LISS-2M equipment for Earth observation, it has a dry mass of 750 kg and a launch mass of 805 kg. IRS-P2 is owned by ISRO and manufactured by ISAC/HAL in India. It is powered by two deployable solar arrays and batteries and uses Active Orbit Control System (AOCS) for motor operations. The satellite achieved an operational lifetime of three years, exceeding its one-year design life.
Physical Characteristics

Length

1.6

Diameter

1.1

Span

12

Dry Mass

750

Launch Mass

805

Shape

Box + 2 Pan

Radar Cross Section

3.5092

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

IRS-P2

Purpose

Earth observation

Mission

Earth observation

Manufacturer

ISAC/HAL

Life Expectancy

1 year (design); 3 years (achieved)

Bus

IRS

Configuration

IRS-1 Bus

Motor

AOCS

Equipment

LISS-2M

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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