IRS-P5 (CARTOSAT-1) (28649)

COSPAR: 2005-017A | Alt Name: Cartosat-1

Image
IRS-P5 (CARTOSAT-1) Satellite Image
Additional Sources
Launch Details

Launch Date

May 5, 2005

Launch Site

SRILR

Launch Pad

SLP

Launch Vehicle

PSLV

Orbital Elements

NORAD ID

28649

International Designator

2005-017A

Epoch

Sat, 04 Jul 2026 01:21:23 GMT

Apogee

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Perigee

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Inclination

97.53°

Right Ascension

207.36°

Eccentricity

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Argument of Perigee

60.39°

Period

96.57 min

Mean Motion

14.91 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-P5 (CARTOSAT-1)

Alternative Name

Cartosat-1

Type

Payload

Status

Operational

Owner

ISRO

Country

India

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 28649U 05017A   26185.05651699  .00001567  00000-0  16347-3 0  9998
2 28649  97.5304 207.3557 0002033  60.3852 299.7569 14.91095228146335

Source: Celestrak

Summary
IRS-P5 (CARTOSAT-1), also known as Cartosat-1, is an Earth observation satellite launched by ISRO on May 5, 2005, from the Satish Dhawan Space Centre using a PSLV launch vehicle. It measures 2.8 meters in length and has a diameter of 2 meters with a span of 12 meters, indicating solar panels or antennas extend beyond its main body. The satellite has a dry mass of 1560 kilograms and was designed to operate for five years. Equipped with PAN Fore and PAN After instruments for high-resolution imagery, Cartosat-1 utilizes two deployable solar arrays and batteries for power generation. Its shape is described as box-like with two pannier structures, and it has a radar cross-section of 4.6921 square meters. The satellite's mission focuses on Earth observation and was operated by ISRO.
Physical Characteristics

Length

2.8

Diameter

2

Span

12

Dry Mass

1560

Launch Mass

1560

Shape

Box + 2 Pan

Radar Cross Section

4.6921

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Cartosat-1

Purpose

Earth observation

Mission

Earth observation

Manufacturer

ISRO

Life Expectancy

5 years

Bus

IRS

Configuration

IRS-1 Bus

Motor

AOCS

Equipment

PAN Fore, PAN After

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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