TKSAT-1 (TUPAC KATARI) (39481)

COSPAR: 2013-075A | Alt Name: Tupac Katari

Image
TKSAT-1 (TUPAC KATARI) Satellite Image
Additional Sources
Launch Details

Launch Date

December 20, 2013

Launch Site

XICLF

Launch Pad

LC2

Launch Vehicle

Chang Zheng 3B

Orbital Elements

NORAD ID

39481

International Designator

2013-075A

Epoch

Sat, 04 Jul 2026 03:12:29 GMT

Apogee

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Perigee

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Inclination

0.04°

Right Ascension

131.67°

Eccentricity

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Argument of Perigee

325.08°

Period

1436.12 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

TKSAT-1 (TUPAC KATARI)

Alternative Name

Tupac Katari

Type

Payload

Status

Operational

Owner

ABE

Country

Bolivia

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 39481U 13075A   26185.13367125 -.00000183  00000-0  00000-0 0  9994
2 39481   0.0395 131.6749 0002681 325.0769 146.3225  1.00270452 45771

Source: Celestrak

Summary
TKSAT-1 (TUPAC KATARI), also known as Tupac Katari or Bolivarsat, is a communication satellite launched on December 20, 2013, from the Xichang Satellite Launch Center using a Chang Zheng 3B launch vehicle. Operated by ABE and manufactured by CAST with the DFH-4 Bus configuration, it has dimensions of 5 meters in length, 2.5 meters in diameter, and spans 30 meters when its solar arrays are deployed. The satellite's dry mass is 2500 kg, while its launch mass was 5086 kg. Equipped with 26 Ku-band, 2 C-band, and 2 Ka-band transponders for communication purposes, TKSAT-1 (TUPAC KATARI) uses two deployable solar arrays and batteries to provide power. It has a designed lifetime of 15 years.
Physical Characteristics

Length

5

Diameter

2.5

Span

30

Dry Mass

2500

Launch Mass

5086

Shape

Box+ 2 panels

Radar Cross Section

40.9678

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Tupac Katari (Bolivarsat)

Purpose

Communication

Mission

Communication

Manufacturer

CAST

Life Expectancy

15 years

Bus

DFH-4

Configuration

DFH-4 Bus

Motor

DFH-4 LAE

Equipment

26 Ku-band, 2 C-band and 2 Ka-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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