IRNSS-1A (39199)

COSPAR: 2013-034A | Alt Name: IRNSS-R1A

Image
IRNSS-1A Satellite Image
Additional Sources
Launch Details

Launch Date

July 1, 2013

Launch Site

SRILR

Launch Pad

FLP

Launch Vehicle

PSLV-XL

Orbital Elements

NORAD ID

39199

International Designator

2013-034A

Epoch

Fri, 03 Jul 2026 17:37:07 GMT

Apogee

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Perigee

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Inclination

35.76°

Right Ascension

63.63°

Eccentricity

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Argument of Perigee

181.68°

Period

1435.98 min

Mean Motion

1.00 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

IRNSS-1A

Alternative Name

IRNSS-R1A

Type

Payload

Status

Partially operational

Owner

ISRO

Country

India

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 39199U 13034A   26184.73411578  .00000069  00000-0  00000-0 0  9994
2 39199  35.7564  63.6330 0017846 181.6829 355.8200  1.00279824 47530

Source: Celestrak

Summary
IRNSS-1A, also known as IRNSS-R1A, is an Indian navigation satellite launched on July 1, 2013, from the Satish Dhawan Space Centre (SRILR) using a PSLV-XL launch vehicle. The spacecraft has dimensions of 1.5 meters in length and diameter, with a span of 10 meters due to its deployable solar arrays. It weighs 614 kg dry and had a launch mass of 1425 kg. IRNSS-1A is equipped with a navigation payload, CDMA ranging payload, and a laser retro-reflector for precise location tracking. The satellite uses ISRO LAM as its motor and has batteries in addition to the solar arrays for power storage. Its mission is to provide navigation services and it was manufactured by Indian Space Research Organisation (ISAC) under the ownership of ISRO. The satellite's expected lifetime is 12 years.
Physical Characteristics

Length

1.5

Diameter

1.5

Span

10

Dry Mass

614

Launch Mass

1425

Shape

Box + 2 Pan

Radar Cross Section

3.4785

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

IRNSS-1A

Purpose

Navigation

Mission

Navigation

Manufacturer

ISAC

Life Expectancy

12 years

Bus

I1K

Configuration

I-1K (I-1000) Bus

Motor

ISRO LAM

Equipment

Navigation payload, CDMA ranging payload, laser retro-reflector

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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