TIRSAT (58989)

COSPAR: 2024-032C | Alt Name: TIRSAT

Image
TIRSAT Satellite Image
Additional Sources
Launch Details

Launch Date

February 17, 2024

Launch Site

TANSC

Launch Pad

Y2

Launch Vehicle

H3-22S

Orbital Elements

NORAD ID

58989

International Designator

2024-032C

Epoch

Sun, 19 Jul 2026 17:24:03 GMT

Apogee

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Perigee

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Inclination

98.00°

Right Ascension

258.55°

Eccentricity

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Argument of Perigee

55.69°

Period

97.79 min

Mean Motion

14.73 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

TIRSAT

Alternative Name

TIRSAT

Type

Payload

Status

Operational

Owner

JSS

Country

Japan

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58989U 24032C   26200.72504115  .00000520  00000+0  89685-4 0  9991
2 58989  97.9950 258.5450 0005903  55.6916 304.4849 14.72528363129878

Source: Celestrak

Summary
TIRSAT is a CubeSat (3U) satellite manufactured by JSS and owned by the same entity. Launched on February 17, 2024, from TANSC Launch Site Y2 using the H3-22S launch vehicle, it has a length of 0.38 meters, diameter of 0.12 meters, and span of 0.8 meters. The satellite weighs 5 kg both at launch and dry mass. Its primary mission is technology demonstration and earth observation, powered by solar cells and batteries. TIRSAT's shape consists of a box with four panels and was designed for these purposes without additional equipment or major events documented.
Physical Characteristics

Length

0.38

Diameter

0.12

Span

0.8

Dry Mass

5

Launch Mass

5

Shape

Box +4 pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

TIRSAT

Purpose

Technology, earth observation

Mission

Technology, earth observation

Manufacturer

JSS

Life Expectancy

?

Bus

Cubesat 3U

Configuration

CubeSat (3U)

Motor

Unknown

Equipment

Unknown

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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