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VeneSat-1: Venezuela's First Satellite

At a Glance

Title: VeneSat-1: Venezuela's First Satellite

Total Categories: 7

Category Stats

  • Satellite Identification and Naming: 2 flashcards, 4 questions
  • Launch and Manufacturing: 5 flashcards, 6 questions
  • Orbital Parameters and Services: 16 flashcards, 13 questions
  • Technical Specifications and Design: 10 flashcards, 12 questions
  • Operational Control and Management: 1 flashcards, 2 questions
  • Mission Failure and Deactivation: 11 flashcards, 18 questions
  • Satellite Cataloging: 4 flashcards, 4 questions

Total Stats

  • Total Flashcards: 50
  • True/False Questions: 29
  • Multiple Choice Questions: 30
  • Total Questions: 59

Instructions

Click the button to expand the instructions for how to use the Wiki2Web Teacher studio in order to print, edit, and export data about VeneSat-1: Venezuela's First Satellite

Welcome to Your Curriculum Command Center

This guide will turn you into a Wiki2web Studio power user. Let's unlock the features designed to give you back your weekends.

The Core Concept: What is a "Kit"?

Think of a Kit as your all-in-one digital lesson plan. It's a single, portable file that contains every piece of content for a topic: your subject categories, a central image, all your flashcards, and all your questions. The true power of the Studio is speed—once a kit is made (or you import one), you are just minutes away from printing an entire set of coursework.

Getting Started is Simple:

  • Create New Kit: Start with a clean slate. Perfect for a brand-new lesson idea.
  • Import & Edit Existing Kit: Load a .json kit file from your computer to continue your work or to modify a kit created by a colleague.
  • Restore Session: The Studio automatically saves your progress in your browser. If you get interrupted, you can restore your unsaved work with one click.

Step 1: Laying the Foundation (The Authoring Tools)

This is where you build the core knowledge of your Kit. Use the left-side navigation panel to switch between these powerful authoring modules.

⚙️ Kit Manager: Your Kit's Identity

This is the high-level control panel for your project.

  • Kit Name: Give your Kit a clear title. This will appear on all your printed materials.
  • Master Image: Upload a custom cover image for your Kit. This is essential for giving your content a professional visual identity, and it's used as the main graphic when you export your Kit as an interactive game.
  • Topics: Create the structure for your lesson. Add topics like "Chapter 1," "Vocabulary," or "Key Formulas." All flashcards and questions will be organized under these topics.

🃏 Flashcard Author: Building the Knowledge Blocks

Flashcards are the fundamental concepts of your Kit. Create them here to define terms, list facts, or pose simple questions.

  • Click "➕ Add New Flashcard" to open the editor.
  • Fill in the term/question and the definition/answer.
  • Assign the flashcard to one of your pre-defined topics.
  • To edit or remove a flashcard, simply use the ✏️ (Edit) or ❌ (Delete) icons next to any entry in the list.

✍️ Question Author: Assessing Understanding

Create a bank of questions to test knowledge. These questions are the engine for your worksheets and exams.

  • Click "➕ Add New Question".
  • Choose a Type: True/False for quick checks or Multiple Choice for more complex assessments.
  • To edit an existing question, click the ✏️ icon. You can change the question text, options, correct answer, and explanation at any time.
  • The Explanation field is a powerful tool: the text you enter here will automatically appear on the teacher's answer key and on the Smart Study Guide, providing instant feedback.

🔗 Intelligent Mapper: The Smart Connection

This is the secret sauce of the Studio. The Mapper transforms your content from a simple list into an interconnected web of knowledge, automating the creation of amazing study guides.

  • Step 1: Select a question from the list on the left.
  • Step 2: In the right panel, click on every flashcard that contains a concept required to answer that question. They will turn green, indicating a successful link.
  • The Payoff: When you generate a Smart Study Guide, these linked flashcards will automatically appear under each question as "Related Concepts."

Step 2: The Magic (The Generator Suite)

You've built your content. Now, with a few clicks, turn it into a full suite of professional, ready-to-use materials. What used to take hours of formatting and copying-and-pasting can now be done in seconds.

🎓 Smart Study Guide Maker

Instantly create the ultimate review document. It combines your questions, the correct answers, your detailed explanations, and all the "Related Concepts" you linked in the Mapper into one cohesive, printable guide.

📝 Worksheet & 📄 Exam Builder

Generate unique assessments every time. The questions and multiple-choice options are randomized automatically. Simply select your topics, choose how many questions you need, and generate:

  • A Student Version, clean and ready for quizzing.
  • A Teacher Version, complete with a detailed answer key and the explanations you wrote.

🖨️ Flashcard Printer

Forget wrestling with table layouts in a word processor. Select a topic, choose a cards-per-page layout, and instantly generate perfectly formatted, print-ready flashcard sheets.

Step 3: Saving and Collaborating

  • 💾 Export & Save Kit: This is your primary save function. It downloads the entire Kit (content, images, and all) to your computer as a single .json file. Use this to create permanent backups and share your work with others.
  • ➕ Import & Merge Kit: Combine your work. You can merge a colleague's Kit into your own or combine two of your lessons into a larger review Kit.

You're now ready to reclaim your time.

You're not just a teacher; you're a curriculum designer, and this is your Studio.

This page is an interactive visualization based on the Wikipedia article "Venesat-1" (opens in new tab) and its cited references.

Text content is available under the Creative Commons Attribution-ShareAlike 4.0 License (opens in new tab). Additional terms may apply.

Disclaimer: This website is for informational purposes only and does not constitute any kind of advice. The information is not a substitute for consulting official sources or records or seeking advice from qualified professionals.


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Study Guide: VeneSat-1: Venezuela's First Satellite

Study Guide: VeneSat-1: Venezuela's First Satellite

Satellite Identification and Naming

VeneSat-1, also known by the name Simón Bolívar, represented Venezuela's inaugural satellite.

Answer: True

VeneSat-1, designated Simón Bolívar, was indeed Venezuela's first satellite, named in honor of the prominent independence leader.

Related Concepts:

  • What was the primary designation and alternative name for Venezuela's first satellite?: Venezuela's first satellite was designated VeneSat-1, and it was also known by the name Simón Bolívar, honoring the prominent Venezuelan independence fighter.
  • Which Venezuelan agency was responsible for operating VeneSat-1?: VeneSat-1 was operated by Venezuela's Bolivarian Agency for Space Activities, commonly referred to by its acronym, ABAE.
  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.

The name Simón Bolívar honors a key figure in the independence movements of North America.

Answer: False

Simón Bolívar was a pivotal leader in the independence movements of South America, not North America.

Related Concepts:

  • What historical figure is honored by the satellite's alternative name, Simón Bolívar?: The name Simón Bolívar honors the pivotal leader of the independence movements in South America against Spanish colonial rule.

What was the primary designation and the alternative name conferred upon Venezuela's first satellite?

Answer: VENESAT-1, Simón Bolívar

Venezuela's inaugural satellite was designated VeneSat-1 and was also known by the name Simón Bolívar, honoring the prominent independence leader.

Related Concepts:

  • What was the primary designation and alternative name for Venezuela's first satellite?: Venezuela's first satellite was designated VeneSat-1, and it was also known by the name Simón Bolívar, honoring the prominent Venezuelan independence fighter.
  • Which Venezuelan agency was responsible for operating VeneSat-1?: VeneSat-1 was operated by Venezuela's Bolivarian Agency for Space Activities, commonly referred to by its acronym, ABAE.
  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.

The alternative name Simón Bolívar honors which historical figure?

Answer: The primary leader of South American independence movements.

The name Simón Bolívar honors the pivotal leader of the South American independence movements against Spanish colonial rule.

Related Concepts:

  • What historical figure is honored by the satellite's alternative name, Simón Bolívar?: The name Simón Bolívar honors the pivotal leader of the independence movements in South America against Spanish colonial rule.

Launch and Manufacturing

The China Aerospace Science and Technology Corporation (CASC) was the sole entity directly responsible for VeneSat-1's design, construction, and launch.

Answer: False

While CASC was involved, its subsidiary, the China Great Wall Industry Corporation (CGWIC), was directly responsible for the design, construction, and launch, indicating CASC was not the *sole* entity.

Related Concepts:

  • What role did the China Aerospace Science and Technology Corporation play in the overall project of VeneSat-1?: The China Aerospace Science and Technology Corporation, through its subsidiary CGWIC, provided comprehensive services for VeneSat-1, encompassing its design, manufacturing, and launch.
  • Which entity was responsible for the design, construction, and launch of VeneSat-1?: The design, construction, and launch of VeneSat-1 were executed by the China Great Wall Industry Corporation (CGWIC), a subsidiary of the China Aerospace Science and Technology Corporation.
  • What was the specific satellite bus model utilized for VeneSat-1?: VeneSat-1 was constructed using the DFH-4 satellite bus model, which was developed by the China Academy of Space Technology.

VeneSat-1 was launched on October 29, 2008, utilizing a Long March 3B carrier rocket.

Answer: True

The launch date of October 29, 2008, and the use of a Long March 3B carrier rocket are confirmed details of VeneSat-1's deployment.

Related Concepts:

  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.
  • What specific variant of the Long March rocket was employed for the launch of VeneSat-1?: The Long March 3B/E model was the specific variant of the Long March rocket used to carry VeneSat-1 into orbit.
  • What information does the COSPAR ID '2008-055A' convey about VeneSat-1?: The COSPAR ID '2008-055A' indicates that VeneSat-1 was the first payload (A) launched in the 55th launch event (055) of the year 2008, according to the Committee on Space Research (COSPAR) numbering system.

The launch of VeneSat-1 occurred at the Wenchang Space Launch Site in China.

Answer: False

VeneSat-1 was launched from the Xichang Satellite Launch Center, not the Wenchang Space Launch Site.

Related Concepts:

  • Which entity was responsible for the design, construction, and launch of VeneSat-1?: The design, construction, and launch of VeneSat-1 were executed by the China Great Wall Industry Corporation (CGWIC), a subsidiary of the China Aerospace Science and Technology Corporation.
  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.
  • What role did the China Aerospace Science and Technology Corporation play in the overall project of VeneSat-1?: The China Aerospace Science and Technology Corporation, through its subsidiary CGWIC, provided comprehensive services for VeneSat-1, encompassing its design, manufacturing, and launch.

Which entity held direct responsibility for the design, construction, and launch of the VeneSat-1 satellite?

Answer: China Great Wall Industry Corporation (CGWIC)

The China Great Wall Industry Corporation (CGWIC), a subsidiary of CASC, was directly responsible for the design, construction, and launch of VeneSat-1.

Related Concepts:

  • Which entity was responsible for the design, construction, and launch of VeneSat-1?: The design, construction, and launch of VeneSat-1 were executed by the China Great Wall Industry Corporation (CGWIC), a subsidiary of the China Aerospace Science and Technology Corporation.
  • What role did the China Aerospace Science and Technology Corporation play in the overall project of VeneSat-1?: The China Aerospace Science and Technology Corporation, through its subsidiary CGWIC, provided comprehensive services for VeneSat-1, encompassing its design, manufacturing, and launch.
  • Which Venezuelan agency was responsible for operating VeneSat-1?: VeneSat-1 was operated by Venezuela's Bolivarian Agency for Space Activities, commonly referred to by its acronym, ABAE.

On what date and time was VeneSat-1 successfully launched into orbit?

Answer: October 29, 2008, 16:53 UTC

VeneSat-1 was successfully launched into orbit on October 29, 2008, at 16:53 UTC.

Related Concepts:

  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.
  • When did VeneSat-1 officially commence its operational service?: VeneSat-1 officially entered service in January 2009, several months after its successful launch in October 2008.
  • What was the epoch date and time recorded for VeneSat-1's orbital parameters?: The epoch, which is a reference point in time for orbital elements, for VeneSat-1's parameters was March 24, 2020, at 05:04:06 UTC.

What specific variant of the Long March rocket was utilized for VeneSat-1's deployment?

Answer: Long March 3B/E

The deployment of VeneSat-1 was accomplished using the Long March 3B/E carrier rocket.

Related Concepts:

  • What specific variant of the Long March rocket was employed for the launch of VeneSat-1?: The Long March 3B/E model was the specific variant of the Long March rocket used to carry VeneSat-1 into orbit.
  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.
  • Which entity was responsible for the design, construction, and launch of VeneSat-1?: The design, construction, and launch of VeneSat-1 were executed by the China Great Wall Industry Corporation (CGWIC), a subsidiary of the China Aerospace Science and Technology Corporation.

Orbital Parameters and Services

VeneSat-1 was classified as a communications satellite intended for operation within a geosynchronous orbit.

Answer: True

The satellite's design and purpose aligned with communications functions, and it was engineered for deployment in a geosynchronous orbit, enabling it to maintain a fixed position relative to Earth.

Related Concepts:

  • What type of satellite was VeneSat-1, and what kind of orbit did it occupy?: VeneSat-1 was a communications satellite designed to operate from a geosynchronous orbit. This orbital configuration allows the satellite to maintain a fixed position relative to a point on Earth's surface.
  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

VeneSat-1 was positioned in an orbital slot at 78° East longitude.

Answer: False

VeneSat-1 was positioned in an orbital slot at 78° West longitude, not East.

Related Concepts:

  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.

The primary services intended for VeneSat-1 included television broadcasting and broadband internet connectivity.

Answer: True

Television broadcasting and broadband internet connectivity were indeed the principal services for which VeneSat-1 was designed and utilized.

Related Concepts:

  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.
  • What types of services were primarily facilitated by VeneSat-1's C-band transponders?: The C-band transponders on VeneSat-1 were utilized to provide communication services, including television broadcasting and broadband connectivity, across the continent of South America.
  • What type of satellite was VeneSat-1, and what kind of orbit did it occupy?: VeneSat-1 was a communications satellite designed to operate from a geosynchronous orbit. This orbital configuration allows the satellite to maintain a fixed position relative to a point on Earth's surface.

VeneSat-1 held strategic importance for amplifying Telesur's broadcast reach and circumventing geo-blocking restrictions.

Answer: True

The satellite facilitated the expansion of Telesur's signal coverage and enabled it to bypass geographical content restrictions.

Related Concepts:

  • What was the strategic significance of VeneSat-1 concerning the regional network Telesur?: VeneSat-1 played a key role in amplifying the reach of Telesur's programming by enabling the network to circumvent geo-blocking restrictions that might have been imposed by service providers.
  • What frequency bands did VeneSat-1 utilize, and what were their respective primary coverage areas?: VeneSat-1 utilized C-band transponders for coverage across South America, while its Ku-band and Ka-band transponders were primarily focused on the Venezuela region.
  • What types of services were primarily facilitated by VeneSat-1's C-band transponders?: The C-band transponders on VeneSat-1 were utilized to provide communication services, including television broadcasting and broadband connectivity, across the continent of South America.

VeneSat-1 officially commenced its operational service in January 2009.

Answer: True

Following its launch in October 2008, VeneSat-1 began its operational service in January 2009.

Related Concepts:

  • When did VeneSat-1 officially commence its operational service?: VeneSat-1 officially entered service in January 2009, several months after its successful launch in October 2008.
  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.

VeneSat-1's geostationary orbit exhibited a very low inclination of approximately 0.0472° relative to the Earth's equator.

Answer: True

The satellite's orbital inclination was indeed very low, measuring approximately 0.0472°, indicating a near-equatorial orbit.

Related Concepts:

  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • What does the term 'orbital inclination' measure concerning a satellite's path?: Orbital inclination measures the angle between a satellite's orbital plane and a reference plane, typically the Earth's equatorial plane. A very low inclination, like VeneSat-1's 0.0472°, indicates that its orbit is nearly aligned with the equator.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

VeneSat-1 utilized its C-band transponders primarily for coverage within the Venezuela region.

Answer: False

While C-band was used, it primarily provided coverage across South America. The Ku-band and Ka-band transponders were focused on the Venezuela region.

Related Concepts:

  • What frequency bands did VeneSat-1 utilize, and what were their respective primary coverage areas?: VeneSat-1 utilized C-band transponders for coverage across South America, while its Ku-band and Ka-band transponders were primarily focused on the Venezuela region.
  • What was the geographical focus for the services provided by VeneSat-1's Ku and Ka-band transponders?: The Ku-band and Ka-band transponders on VeneSat-1 were primarily directed towards serving the Venezuela region.
  • What types of services were primarily facilitated by VeneSat-1's C-band transponders?: The C-band transponders on VeneSat-1 were utilized to provide communication services, including television broadcasting and broadband connectivity, across the continent of South America.

What type of orbit was VeneSat-1 designed to occupy to maintain a fixed position relative to Earth?

Answer: Geosynchronous Orbit

VeneSat-1 was designed for a geosynchronous orbit, which allows a satellite to maintain a consistent position relative to a specific point on Earth's surface.

Related Concepts:

  • What type of satellite was VeneSat-1, and what kind of orbit did it occupy?: VeneSat-1 was a communications satellite designed to operate from a geosynchronous orbit. This orbital configuration allows the satellite to maintain a fixed position relative to a point on Earth's surface.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

At which West longitude was VeneSat-1 positioned in its designated geostationary orbital slot?

Answer: 78° West

VeneSat-1 was positioned in a geostationary orbital slot located at 78° West longitude.

Related Concepts:

  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

Which of the following was identified as a primary service provided by VeneSat-1?

Answer: Television broadcasting

Television broadcasting was one of the primary services intended for VeneSat-1.

Related Concepts:

  • What was the intended operational lifespan for VeneSat-1?: VeneSat-1 was designed with an expected service life of 15 years.
  • What type of satellite was VeneSat-1, and what kind of orbit did it occupy?: VeneSat-1 was a communications satellite designed to operate from a geosynchronous orbit. This orbital configuration allows the satellite to maintain a fixed position relative to a point on Earth's surface.
  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.

What strategic advantage did VeneSat-1 provide for the regional network Telesur?

Answer: It enabled Telesur to circumvent geo-blocking restrictions.

VeneSat-1 provided Telesur with the strategic advantage of circumventing geo-blocking restrictions, thereby expanding its broadcast reach.

Related Concepts:

  • What was the strategic significance of VeneSat-1 concerning the regional network Telesur?: VeneSat-1 played a key role in amplifying the reach of Telesur's programming by enabling the network to circumvent geo-blocking restrictions that might have been imposed by service providers.
  • What frequency bands did VeneSat-1 utilize, and what were their respective primary coverage areas?: VeneSat-1 utilized C-band transponders for coverage across South America, while its Ku-band and Ka-band transponders were primarily focused on the Venezuela region.
  • What types of services were primarily facilitated by VeneSat-1's C-band transponders?: The C-band transponders on VeneSat-1 were utilized to provide communication services, including television broadcasting and broadband connectivity, across the continent of South America.

Which frequency band was primarily utilized by VeneSat-1 for coverage across South America?

Answer: C-band

The C-band transponders on VeneSat-1 were primarily employed for providing coverage across the South American continent.

Related Concepts:

  • What frequency bands did VeneSat-1 utilize, and what were their respective primary coverage areas?: VeneSat-1 utilized C-band transponders for coverage across South America, while its Ku-band and Ka-band transponders were primarily focused on the Venezuela region.
  • What types of services were primarily facilitated by VeneSat-1's C-band transponders?: The C-band transponders on VeneSat-1 were utilized to provide communication services, including television broadcasting and broadband connectivity, across the continent of South America.
  • What was the geographical focus for the services provided by VeneSat-1's Ku and Ka-band transponders?: The Ku-band and Ka-band transponders on VeneSat-1 were primarily directed towards serving the Venezuela region.

Why is a satellite drifting from its assigned geostationary orbital position considered a significant problem?

Answer: It can cause interference with other satellites and disrupt service areas.

Drifting from its assigned geostationary position is problematic because it can lead to interference with other satellites and disrupt the intended service coverage areas.

Related Concepts:

  • Why is a satellite drifting from its assigned orbital position considered a significant issue?: Satellites in geostationary orbit are assigned specific longitude slots to ensure continuous coverage over particular regions. If a satellite drifts, it deviates from its designated position, disrupting its intended service area and potentially causing interference with other satellites operating nearby.

Technical Specifications and Design

The satellite bus model employed for VeneSat-1 was the DFH-3, developed by the China Academy of Space Technology.

Answer: False

VeneSat-1 utilized the DFH-4 satellite bus model, not the DFH-3. The DFH-4 was developed by the China Academy of Space Technology (CAST).

Related Concepts:

  • Who manufactured the DFH-4 satellite bus that served as the platform for VeneSat-1?: The DFH-4 satellite bus, which formed the structural and systems foundation for VeneSat-1, was manufactured by the China Academy of Space Technology.
  • What was the specific satellite bus model utilized for VeneSat-1?: VeneSat-1 was constructed using the DFH-4 satellite bus model, which was developed by the China Academy of Space Technology.
  • What is the function of a 'satellite bus' in spacecraft engineering?: A satellite bus, such as the DFH-4 used for VeneSat-1, provides the fundamental infrastructure for the satellite. It includes essential systems like power generation and distribution, propulsion, attitude control, thermal management, and command and data handling, which support the satellite's payload.

The total launch mass of VeneSat-1 was approximately 11,131 pounds.

Answer: True

The satellite's launch mass is documented as approximately 11,131 pounds, which is equivalent to 5,049 kilograms.

Related Concepts:

  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.
  • What were the physical dimensions of the VeneSat-1 satellite?: VeneSat-1 measured approximately 2.36 meters in length, 2.1 meters in width, and 4 meters in height, translating to roughly 7.7 by 6.9 by 13.1 feet.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.

VeneSat-1 was designed with an intended operational lifespan of 20 years.

Answer: False

The intended operational lifespan for VeneSat-1 was 15 years, not 20 years.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the intended operational lifespan for VeneSat-1?: VeneSat-1 was designed with an expected service life of 15 years.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.

VeneSat-1's payload included transponders operating in the C-band, Ku-band, and X-band frequencies.

Answer: False

VeneSat-1's payload included C-band, Ku-band, and Ka-band transponders. It did not include X-band transponders.

Related Concepts:

  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.
  • What frequency bands did VeneSat-1 utilize, and what were their respective primary coverage areas?: VeneSat-1 utilized C-band transponders for coverage across South America, while its Ku-band and Ka-band transponders were primarily focused on the Venezuela region.
  • What was the geographical focus for the services provided by VeneSat-1's Ku and Ka-band transponders?: The Ku-band and Ka-band transponders on VeneSat-1 were primarily directed towards serving the Venezuela region.

What satellite bus model served as the structural and systems foundation for VeneSat-1?

Answer: DFH-4

The DFH-4 satellite bus model provided the structural and systems foundation for VeneSat-1.

Related Concepts:

  • What was the specific satellite bus model utilized for VeneSat-1?: VeneSat-1 was constructed using the DFH-4 satellite bus model, which was developed by the China Academy of Space Technology.
  • Who manufactured the DFH-4 satellite bus that served as the platform for VeneSat-1?: The DFH-4 satellite bus, which formed the structural and systems foundation for VeneSat-1, was manufactured by the China Academy of Space Technology.
  • What is the function of a 'satellite bus' in spacecraft engineering?: A satellite bus, such as the DFH-4 used for VeneSat-1, provides the fundamental infrastructure for the satellite. It includes essential systems like power generation and distribution, propulsion, attitude control, thermal management, and command and data handling, which support the satellite's payload.

What was the approximate launch mass of the VeneSat-1 satellite, expressed in kilograms?

Answer: 5,049 kg

The approximate launch mass of VeneSat-1 was 5,049 kilograms (equivalent to approximately 11,131 pounds).

Related Concepts:

  • What were the physical dimensions of the VeneSat-1 satellite?: VeneSat-1 measured approximately 2.36 meters in length, 2.1 meters in width, and 4 meters in height, translating to roughly 7.7 by 6.9 by 13.1 feet.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • On what date and time was VeneSat-1 launched, and what rocket was used for its deployment?: VeneSat-1 was launched on October 29, 2008, at 16:53 UTC, utilizing a Chinese Long March 3B carrier rocket.

What was the intended operational lifespan designed for the VeneSat-1 satellite?

Answer: 15 years

VeneSat-1 was designed with an intended operational lifespan of 15 years.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the intended operational lifespan for VeneSat-1?: VeneSat-1 was designed with an expected service life of 15 years.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.

How many Ka-band transponders were included in VeneSat-1's communication payload?

Answer: 2

VeneSat-1's communication payload included two Ka-band transponders.

Related Concepts:

  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.
  • What frequency bands did VeneSat-1 utilize, and what were their respective primary coverage areas?: VeneSat-1 utilized C-band transponders for coverage across South America, while its Ku-band and Ka-band transponders were primarily focused on the Venezuela region.
  • What was the geographical focus for the services provided by VeneSat-1's Ku and Ka-band transponders?: The Ku-band and Ka-band transponders on VeneSat-1 were primarily directed towards serving the Venezuela region.

Which organization manufactured the DFH-4 satellite bus platform utilized for VeneSat-1?

Answer: China Academy of Space Technology (CAST)

The DFH-4 satellite bus platform for VeneSat-1 was manufactured by the China Academy of Space Technology (CAST).

Related Concepts:

  • Who manufactured the DFH-4 satellite bus that served as the platform for VeneSat-1?: The DFH-4 satellite bus, which formed the structural and systems foundation for VeneSat-1, was manufactured by the China Academy of Space Technology.
  • What was the specific satellite bus model utilized for VeneSat-1?: VeneSat-1 was constructed using the DFH-4 satellite bus model, which was developed by the China Academy of Space Technology.
  • What is the function of a 'satellite bus' in spacecraft engineering?: A satellite bus, such as the DFH-4 used for VeneSat-1, provides the fundamental infrastructure for the satellite. It includes essential systems like power generation and distribution, propulsion, attitude control, thermal management, and command and data handling, which support the satellite's payload.

What was the approximate physical height of the VeneSat-1 satellite?

Answer: 4 meters

The approximate physical height of the VeneSat-1 satellite was 4 meters.

Related Concepts:

  • What were the physical dimensions of the VeneSat-1 satellite?: VeneSat-1 measured approximately 2.36 meters in length, 2.1 meters in width, and 4 meters in height, translating to roughly 7.7 by 6.9 by 13.1 feet.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

What was the power generation capacity of the VeneSat-1 satellite?

Answer: 7.75 kilowatts (kW)

The VeneSat-1 satellite had a power generation capacity of 7.75 kilowatts (kW).

Related Concepts:

  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • What were the physical dimensions of the VeneSat-1 satellite?: VeneSat-1 measured approximately 2.36 meters in length, 2.1 meters in width, and 4 meters in height, translating to roughly 7.7 by 6.9 by 13.1 feet.

What is the fundamental function of a transponder aboard a satellite such as VeneSat-1?

Answer: To receive, amplify, and re-transmit signals.

The fundamental function of a transponder is to receive signals, amplify them, and then re-transmit them back to Earth, facilitating communication.

Related Concepts:

  • What is the function of a 'transponder' aboard a satellite?: A transponder is a critical component on a satellite that receives signals on one frequency, amplifies them, and then re-transmits them on a different frequency back to Earth. These devices are essential for relaying various forms of communication.
  • Could you describe the transponder payload carried by VeneSat-1?: VeneSat-1's payload included 14 transponders operating in the C-band, 12 transponders in the Ku-band, and 2 transponders in the Ka-band, enabling various communication services.
  • What types of services were primarily facilitated by VeneSat-1's C-band transponders?: The C-band transponders on VeneSat-1 were utilized to provide communication services, including television broadcasting and broadband connectivity, across the continent of South America.

Operational Control and Management

Venezuela's Bolivarian Agency for Space Activities (ABAE) held responsibility for the operational control of VeneSat-1.

Answer: True

The Bolivarian Agency for Space Activities (ABAE) was designated as the entity responsible for the operational management and control of the VeneSat-1 satellite.

Related Concepts:

  • Which Venezuelan agency was responsible for operating VeneSat-1?: VeneSat-1 was operated by Venezuela's Bolivarian Agency for Space Activities, commonly referred to by its acronym, ABAE.
  • What was the primary designation and alternative name for Venezuela's first satellite?: Venezuela's first satellite was designated VeneSat-1, and it was also known by the name Simón Bolívar, honoring the prominent Venezuelan independence fighter.
  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.

Which Venezuelan agency was responsible for the operational control and management of VeneSat-1?

Answer: Bolivarian Agency for Space Activities (ABAE)

The Bolivarian Agency for Space Activities (ABAE) was tasked with the operational control and management of the VeneSat-1 satellite.

Related Concepts:

  • Which Venezuelan agency was responsible for operating VeneSat-1?: VeneSat-1 was operated by Venezuela's Bolivarian Agency for Space Activities, commonly referred to by its acronym, ABAE.
  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.
  • What was the primary designation and alternative name for Venezuela's first satellite?: Venezuela's first satellite was designated VeneSat-1, and it was also known by the name Simón Bolívar, honoring the prominent Venezuelan independence fighter.

Mission Failure and Deactivation

VeneSat-1 began experiencing significant operational issues around March 13, 2020.

Answer: True

The satellite's operational difficulties commenced approximately on March 13, 2020, marking the beginning of its deactivation phase.

Related Concepts:

  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

The failure of VeneSat-1 was attributed to the loss of its primary communication antenna shortly after launch.

Answer: False

The failure was not due to a communication antenna issue shortly after launch, but rather a loss of power resulting from issues with its solar array drives later in its mission.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.

An emergency maneuver to move VeneSat-1 to a graveyard orbit was successfully completed before the satellite became uncontrollable.

Answer: False

The attempted maneuver to move VeneSat-1 to a graveyard orbit was not successfully completed; the satellite became uncontrollable due to power loss and tumbling.

Related Concepts:

  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.
  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.

As of March 23, 2020, VeneSat-1 was observed in an unstable orbital configuration, having drifted significantly westward from its designated geostationary position.

Answer: False

As of March 23, 2020, VeneSat-1 was not in a stable geostationary orbit; it was observed in an elliptical orbit and had drifted significantly westward.

Related Concepts:

  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.
  • What type of satellite was VeneSat-1, and what kind of orbit did it occupy?: VeneSat-1 was a communications satellite designed to operate from a geosynchronous orbit. This orbital configuration allows the satellite to maintain a fixed position relative to a point on Earth's surface.

Venezuela's Ministry of Science and Technology officially declared VeneSat-1 lost on March 25, 2020.

Answer: True

The official declaration of VeneSat-1 as lost by Venezuela's Ministry of Science and Technology occurred on March 25, 2020.

Related Concepts:

  • On what date did the Venezuelan government officially declare VeneSat-1 lost?: Venezuela's Ministry of Science and Technology officially declared the satellite lost on March 25, 2020, marking the definitive end of its mission.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • Which Venezuelan agency was responsible for operating VeneSat-1?: VeneSat-1 was operated by Venezuela's Bolivarian Agency for Space Activities, commonly referred to by its acronym, ABAE.

VeneSat-1's mission duration exceeded its planned operational lifespan by approximately three years.

Answer: False

VeneSat-1's operational mission duration fell short of its planned lifespan by approximately three years, failing before its intended end of life.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.

The actual operational mission duration of VeneSat-1 was 11 years, 4 months, and 24 days.

Answer: True

The satellite remained operational for a total period of 11 years, 4 months, and 24 days.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the intended operational lifespan for VeneSat-1?: VeneSat-1 was designed with an expected service life of 15 years.
  • When did VeneSat-1 officially commence its operational service?: VeneSat-1 officially entered service in January 2009, several months after its successful launch in October 2008.

The end-of-mission status for VeneSat-1 was officially classified as 'Decommissioned'.

Answer: False

The official end-of-mission status for VeneSat-1 was classified as 'Loss of spacecraft,' not 'Decommissioned'.

Related Concepts:

  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.

Following VeneSat-1's operational failure, its communication functions were transferred to the satellite Intelsat 14.

Answer: True

On March 24, 2020, the majority of VeneSat-1's communication functions were transferred to the Intelsat 14 satellite.

Related Concepts:

  • What happened to VeneSat-1's communication functions after it became inoperable?: Following VeneSat-1's operational failure, the majority of its communication functions were transferred to the American satellite Intelsat 14 on March 24, 2020.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.

Approximately when did VeneSat-1 begin to experience significant operational failures leading to its deactivation?

Answer: March 13, 2020

Significant operational failures, marking the beginning of its deactivation, commenced for VeneSat-1 around March 13, 2020.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.

What technical issue was identified as the direct cause of VeneSat-1 losing power and becoming inoperable?

Answer: Loss of both solar array drives.

The direct cause of VeneSat-1 losing power and becoming inoperable was the loss of both its solar array drives.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.

What emergency procedure was attempted for VeneSat-1 following its operational failures?

Answer: Attempt to move the spacecraft to a graveyard orbit.

An emergency maneuver was attempted to move the spacecraft into a graveyard orbit subsequent to its operational failures.

Related Concepts:

  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the official classification for the disposal or end-of-mission status of VeneSat-1?: The end-of-mission status for VeneSat-1 was recorded as a 'Loss of spacecraft'.

As of March 23, 2020, what was the orbital status of VeneSat-1?

Answer: It was in an elliptical orbit and had drifted significantly westward.

By March 23, 2020, VeneSat-1 was observed in an elliptical orbit and had drifted significantly westward from its intended geostationary position.

Related Concepts:

  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.
  • What was the epoch date and time recorded for VeneSat-1's orbital parameters?: The epoch, which is a reference point in time for orbital elements, for VeneSat-1's parameters was March 24, 2020, at 05:04:06 UTC.

On what date did the Venezuelan government officially declare the VeneSat-1 satellite lost?

Answer: March 25, 2020

The Venezuelan government, through its Ministry of Science and Technology, officially declared VeneSat-1 lost on March 25, 2020.

Related Concepts:

  • On what date did the Venezuelan government officially declare VeneSat-1 lost?: Venezuela's Ministry of Science and Technology officially declared the satellite lost on March 25, 2020, marking the definitive end of its mission.
  • What was the designated orbital slot for VeneSat-1, and how was this position acquired?: VeneSat-1 was positioned in an orbital slot at 78° West longitude. This specific geostationary slot had been originally designated for Uruguay but was subsequently ceded to Venezuela through a mutual agreement.
  • What was the primary designation and alternative name for Venezuela's first satellite?: Venezuela's first satellite was designated VeneSat-1, and it was also known by the name Simón Bolívar, honoring the prominent Venezuelan independence fighter.

How did VeneSat-1's actual operational duration compare to its planned 15-year lifespan?

Answer: It failed about 3 years before its planned end of life.

VeneSat-1's operational mission concluded approximately three years prior to its planned 15-year lifespan.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the intended operational lifespan for VeneSat-1?: VeneSat-1 was designed with an expected service life of 15 years.
  • When did VeneSat-1 begin to experience significant operational issues leading to its deactivation?: VeneSat-1 went out of service starting around March 13, 2020, indicating the beginning of its operational failure.

What was the total duration VeneSat-1 remained operational, expressed in years, months, and days?

Answer: 11 years, 4 months, 24 days

VeneSat-1's total operational mission duration was 11 years, 4 months, and 24 days.

Related Concepts:

  • How did VeneSat-1's mission duration compare to its planned operational lifespan?: VeneSat-1 failed approximately three years prior to its originally planned end of life, which was projected to be 15 years after its launch.
  • What was the intended operational lifespan for VeneSat-1?: VeneSat-1 was designed with an expected service life of 15 years.
  • When did VeneSat-1 officially commence its operational service?: VeneSat-1 officially entered service in January 2009, several months after its successful launch in October 2008.

What is the purpose of maneuvering a satellite into a 'graveyard orbit' at the end of its mission?

Answer: To store decommissioned satellites safely away from active orbits.

Maneuvering a satellite into a graveyard orbit serves to safely store decommissioned spacecraft, thereby preventing collisions and reducing debris in active operational orbits.

Related Concepts:

  • What is the purpose of maneuvering a satellite into a 'graveyard orbit'?: A graveyard orbit is a designated orbital region, usually situated above the operational geostationary belt, where satellites are moved at the end of their service life. This practice helps to prevent collisions with active satellites and mitigates the accumulation of space debris in valuable operational orbits.

What does it signify when a satellite, such as VeneSat-1, is described as 'tumbling' in orbit?

Answer: It is rotating in an uncontrolled manner around multiple axes.

A satellite described as 'tumbling' is rotating in an uncontrolled manner around multiple axes, which severely impairs its operational capabilities.

Related Concepts:

  • What does it mean for a satellite to be 'tumbling' in orbit?: When a satellite is described as 'tumbling,' it indicates that it is rotating in an uncontrolled manner around multiple axes. This uncontrolled rotation makes it extremely difficult to maintain proper orientation for its communication antennas, solar panels, or scientific instruments.
  • What does the term 'orbital inclination' measure concerning a satellite's path?: Orbital inclination measures the angle between a satellite's orbital plane and a reference plane, typically the Earth's equatorial plane. A very low inclination, like VeneSat-1's 0.0472°, indicates that its orbit is nearly aligned with the equator.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.

Satellite Cataloging

The official COSPAR ID assigned to VeneSat-1 is 2008-055B.

Answer: False

The official COSPAR ID for VeneSat-1 is 2008-055A, not 2008-055B.

Related Concepts:

  • What is the official COSPAR ID assigned to the VeneSat-1 satellite?: The international designation, or COSPAR ID, assigned to VeneSat-1 is 2008-055A.
  • What information does the COSPAR ID '2008-055A' convey about VeneSat-1?: The COSPAR ID '2008-055A' indicates that VeneSat-1 was the first payload (A) launched in the 55th launch event (055) of the year 2008, according to the Committee on Space Research (COSPAR) numbering system.
  • What is the SATCAT number associated with the VeneSat-1 satellite?: The satellite catalog number, often abbreviated as SATCAT no., for VeneSat-1 is 33414.

The SATCAT number associated with VeneSat-1 is 33414.

Answer: True

The satellite catalog number, commonly known as SATCAT number, for VeneSat-1 is indeed 33414.

Related Concepts:

  • What is the SATCAT number associated with the VeneSat-1 satellite?: The satellite catalog number, often abbreviated as SATCAT no., for VeneSat-1 is 33414.
  • What is the official COSPAR ID assigned to the VeneSat-1 satellite?: The international designation, or COSPAR ID, assigned to VeneSat-1 is 2008-055A.
  • What information does the COSPAR ID '2008-055A' convey about VeneSat-1?: The COSPAR ID '2008-055A' indicates that VeneSat-1 was the first payload (A) launched in the 55th launch event (055) of the year 2008, according to the Committee on Space Research (COSPAR) numbering system.

The epoch date for VeneSat-1's orbital parameters was recorded as March 24, 2020.

Answer: True

The reference point in time, or epoch, for VeneSat-1's orbital elements was March 24, 2020.

Related Concepts:

  • What was the epoch date and time recorded for VeneSat-1's orbital parameters?: The epoch, which is a reference point in time for orbital elements, for VeneSat-1's parameters was March 24, 2020, at 05:04:06 UTC.
  • What was the approximate final orbital configuration of VeneSat-1 as of late March 2020?: As of March 23, 2020, VeneSat-1 was observed to be in an elliptical orbit, with altitudes ranging between approximately 35,800 and 36,300 kilometers. Additionally, it had drifted approximately 30 degrees westward from its intended geostationary position.
  • Can you detail the key orbital parameters of VeneSat-1 in its geostationary orbit?: In its geostationary orbit, VeneSat-1 maintained a semi-major axis of 42,448.3 km, an eccentricity of 0.0056487, a perigee altitude of 35,830.4 km, an apogee altitude of 36,309.9 km, and an inclination of 0.0472° relative to the Earth's equatorial plane.

What information is conveyed by VeneSat-1's COSPAR ID '2008-055A'?

Answer: It was the first payload launched during the 55th mission event of 2008.

The COSPAR ID '2008-055A' signifies that VeneSat-1 was the first payload (A) launched during the 55th launch event (055) of the year 2008.

Related Concepts:

  • What is the official COSPAR ID assigned to the VeneSat-1 satellite?: The international designation, or COSPAR ID, assigned to VeneSat-1 is 2008-055A.
  • What information does the COSPAR ID '2008-055A' convey about VeneSat-1?: The COSPAR ID '2008-055A' indicates that VeneSat-1 was the first payload (A) launched in the 55th launch event (055) of the year 2008, according to the Committee on Space Research (COSPAR) numbering system.
  • What is the SATCAT number associated with the VeneSat-1 satellite?: The satellite catalog number, often abbreviated as SATCAT no., for VeneSat-1 is 33414.

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