ICON (44628)

COSPAR: 2019-068A | Alt Name: ICON

Image
ICON Satellite Image
Additional Sources
Launch Details

Launch Date

October 11, 2019

Launch Site

ERAS

Launch Pad

RW13

Launch Vehicle

Pegasus XL

Orbital Elements

NORAD ID

44628

International Designator

2019-068A

Epoch

Fri, 03 Jul 2026 22:01:57 GMT

Apogee

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Perigee

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Inclination

26.98°

Right Ascension

271.39°

Eccentricity

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Argument of Perigee

40.62°

Period

95.55 min

Mean Motion

15.07 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

ICON

Alternative Name

ICON

Type

Payload

Status

Non-operational

Owner

GSFC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 44628U 19068A   26184.91802560  .00004260  00000-0  26122-3 0  9998
2 44628  26.9840 271.3892 0013739  40.6235 319.5350 15.07066998368565

Source: Celestrak

Summary
The ICON satellite (NORAD CAT ID: 44628) is a research spacecraft designed to study the ionosphere. Launched on October 11, 2019, from ERAS using a Pegasus XL launch vehicle, it has a configuration known as LEOStar-2 and measures approximately 1.9 meters in length with a diameter of 1.1 meters and a span of 3.6 meters. The satellite's dry mass is 288 kg, identical to its launch mass. ICON is equipped with instruments such as MIGHTI, EUV, FUV, and IVM for scientific research purposes. Its power supply includes two deployable solar arrays and batteries. Manufactured by NGISD, the spacecraft has a design lifetime of 2 years and belongs to GSFC (Goddard Space Flight Center). The shape of the satellite is described as "Hex cyl+cyl+1 pan".
Physical Characteristics

Length

1.9

Diameter

1.1

Span

3.6

Dry Mass

288

Launch Mass

288

Shape

Hex cyl+cyl+1 pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

ICON

Purpose

Research, ionosphere

Mission

Research, ionosphere

Manufacturer

NGISD

Life Expectancy

2 years (design)

Bus

Leostar-2/750

Configuration

LEOStar-2

Motor

AOCS

Equipment

MIGHTI, EUV, FUV, IVM

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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