ZACUBE-1 (TSHEPISOSAT) (39417)

COSPAR: 2013-066B | Alt Name: TshepisoSat

Image
ZACUBE-1 (TSHEPISOSAT) Satellite Image
Additional Sources
Launch Details

Launch Date

November 21, 2013

Launch Site

DLS

Launch Pad

Sh370/13

Launch Vehicle

Dnepr

Orbital Elements

NORAD ID

39417

International Designator

2013-066B

Epoch

Fri, 03 Jul 2026 22:29:51 GMT

Apogee

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Perigee

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Inclination

97.80°

Right Ascension

147.36°

Eccentricity

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Argument of Perigee

191.41°

Period

95.92 min

Mean Motion

15.01 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

ZACUBE-1 (TSHEPISOSAT)

Alternative Name

TshepisoSat

Type

Payload

Status

Operational

Owner

CPUT

Country

South Africa

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 39417U 13066B   26184.93739966  .00003964  00000-0  30713-3 0  9992
2 39417  97.8036 147.3589 0043122 191.4127 168.6124 15.01282961683249

Source: Celestrak

Summary
ZACUBE-1 (TSHEPISOSAT), also known as TshepisoSat, is a CubeSat 1U technology satellite launched on November 21, 2013, from the Dnepr launch vehicle at Sh370/13. The spacecraft has dimensions of 0.1 meters in length, diameter, and span, with a dry mass of 1.2 kg and a launch mass of 1.2 kg as well. It was manufactured by CPUT (Central University of Technology) in South Africa for technology demonstration purposes. ZACUBE-1 is equipped with solar cells and batteries for power and has a shape described as box-like, with a radar cross-section (RCS) of 0.069 square meters. The satellite does not have any specified equipment or major events listed, and it was launched from DLS (Dombarovsky Launch Site).
Physical Characteristics

Length

0.1

Diameter

0.1

Span

0.1

Dry Mass

1.2

Launch Mass

1.2

Shape

Box

Radar Cross Section

0.069

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

ZACUBE-1

Purpose

Technology

Mission

Technology

Manufacturer

CPUT

Life Expectancy

Unknown

Bus

Cubesat 1U

Configuration

CubeSat (1U)

Motor

None

Equipment

Unknown

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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