BEGIN:VCALENDAR VERSION:2.0 PRODID:-//chikkutakku.com//RDFCal 1.0//EN X-WR-CALDESC:GoogleカレンダーやiCalendar形式情報を共有シェ アしましょう。近所のイベントから全国のイベントま で今日のイベント検索やスケジュールを決めるならち っくたっく X-WR-CALNAME:ちっくたっく X-WR-TIMEZONE:UTC BEGIN:VEVENT SUMMARY:Long March CZ-10B • Test Flight DTSTART;VALUE=DATE-TIME:20260710T041000Z DTEND;VALUE=DATE-TIME:20260710T041000Z UID:146368572644 DESCRIPTION:A China Rocket (CALT) Long March (Chang Zheng) CZ-10B rocket will launch on its first test flight. The first stage is powered by seven YF-100N keroLOX engines\, the second stage is propelled by a YF-219 methaL OX engine. The first stage is reusable and will attempt a landing on the d rone ship Linghangzhe (领航者)\, via its tension wires recovery system on its deck.\n-\nDelayed from Apr. 5\, 19\, late April and May.\n\nWebcast : https://www.youtube.com/live/QOT4CBR6ryg\nhttps://www.youtube.com/live/ 8AbjhtpbOv8 LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf kosKTdhF5khDg8 END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260711T020000Z DTEND;VALUE=DATE-TIME:20260711T020000Z UID:337425963038 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 24 Sta rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in ternally known as Starlink Group 17-48 and the booster is designated as B 1097.11 for this mission\, flying with a reused fairing.\n-\nStarlink v2 M ini Optimized satellites are built by SpaceX and have a reported launch ma ss of 575kg. The mass-produced spacecraft carry a communications payload u sing the Ku and Ka frequency bands\, plus E-band for backhaul\, which will allow Starlink to provide ~4x more capacity per satellite than earlier it erations. They also employ optical inter-satellite links\, phased array be am forming and digital processing technologies. On the v2 sats the Krypton thrusters are replaced with new and more powerful Argon Hall thrusters. T he Optimized chassis features upgrades\, such as a new backhaul antenna wi th a SpaceX-designed and built dual-band chip and improved avionics\, prop ulsion and power systems. Starlink sats are able to track on-orbit debris and capable of autonomous collision avoidance. All satellites will be equi pped with anti-reflective coatings.\nThe updated Starlink network architec ture has 1584 satellites at 550km altitude and an inclination of 53 degree s\, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 sate llites at 570km and an inclination of 70 degrees\, and 520 satellites at 5 60km and an inclination of 97.6 degrees. The initial FCC application cover ed 4408 Starlink satellites. Eventually SpaceX will launch and operate a f ollow-on network of 7518 additional Starlink satellites transmitting in V- band frequencies. In the final deployment stage an additional 30000 Starli nk satellites might get orbited.\n-\nDelayed from July 10.\n\nWebcast: \n https://www.spacex.com/launches/sl-17-48\n\nhttps://spaceflightnow.com LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Gravity YL-1 • Fengxing 1 DTSTART;VALUE=DATE-TIME:20260712T030000Z DTEND;VALUE=DATE-TIME:20260712T030000Z UID:614081403447 DESCRIPTION:An Orienspace Gravity 1 rocket will fly on its third flight ca rrying satellites into orbit. The rocket will perform a sea launch from t he Dongfang Hangtiangang (东方航天港号) ship in the Yellow Sea near Haiyang. One of the payloads will be Fengxing 1 (锋行一号). Gravity 1 (引力一号 or Yinli 1) is an all solid rocket with four boosters\, whic h will be capable of land and sea launches. For liftoff only the boosters ignite\, with the core stage getting lit shortly before booster separation .\n-\nDelayed from November 2024\, December 2025 and June 10. LOCATION:Gelbes Meer END:VEVENT BEGIN:VEVENT SUMMARY:Vikram I • Solaras S3 & Scope DTSTART;VALUE=DATE-TIME:20260712T050000Z DTEND;VALUE=DATE-TIME:20260712T090000Z UID:201731902093 DESCRIPTION:A Skyroot Aerospace Vikram I rocket will launch on its first t est flight. It will attempt to carry four CubeSats\, two hosted payloads a nd two ornamental payloads to orbit. CubeSats on this flight are Solaras S 3 and Scope. Solaras S3 will validate Grahaa's nanosatellite bus and other subsystems\, and transmit images taken by its optical payload via SSTV si gnals. Grahaa Space is developing a nano satellite constellation for Earth observation. Hosted payloads are Embrace\, which is a robotic-arm tech de monstrator. It is developed by Hyderabad-based Cosmoserve Space for active space debris removal applications. The other hosted payload package is uD 3PP & mD3RN by DCUBED Space. The mission is named "Aagaman" by Skyroot. Th e four stage Vikram I rocket uses three solid stages (Kalam 1200\, 250\, 1 00) and a hypergolic fueled upper stage propelled by a Raman-2 engine.\n-\ nDelayed from February\, Q2 2024\, September and February. LOCATION:First Launchpad\, P6MM+8V Dhawan Space Centre\, Satish\, Mobile S tructure Tower\, Sriharikota\, Shar Project\, Andhra Pradesh 524124\, Indi en END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260713T080000Z DTEND;VALUE=DATE-TIME:20260713T080000Z UID:119569153878 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 24? St arlink v2 Mini Optimized satellites into low Earth orbit. This flight is i nternally known as Starlink Group 15-13 and the booster is designated as B 10XX.X for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mi ni Optimized satellites are built by SpaceX and have a reported launch mas s of 575kg. The mass-produced spacecraft carry a communications payload us ing the Ku and Ka frequency bands\, plus E-band for backhaul\, which will allow Starlink to provide ~4x more capacity per satellite than earlier ite rations. They also employ optical inter-satellite links\, phased array bea m forming and digital processing technologies. On the v2 sats the Krypton thrusters are replaced with new and more powerful Argon Hall thrusters. Th e Optimized chassis features upgrades\, such as a new backhaul antenna wit h a SpaceX-designed and built dual-band chip and improved avionics\, propu lsion and power systems. Starlink sats are able to track on-orbit debris a nd capable of autonomous collision avoidance. All satellites will be equip ped with anti-reflective coatings.\nThe updated Starlink network architect ure has 1584 satellites at 550km altitude and an inclination of 53 degrees \, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satel lites at 570km and an inclination of 70 degrees\, and 520 satellites at 56 0km and an inclination of 97.6 degrees. The initial FCC application covere d 4408 Starlink satellites. Eventually SpaceX will launch and operate a fo llow-on network of 7518 additional Starlink satellites transmitting in V-b and frequencies. In the final deployment stage an additional 30000 Starlin k satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/laun ches/sl-15-14 LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:Soyuz 2.1a • Soyuz MS-29 / ISS 75S DTSTART;VALUE=DATE-TIME:20260714T144700Z DTEND;VALUE=DATE-TIME:20260714T144700Z UID:238280944189 DESCRIPTION:A RKTs Progress Soyuz 2.1a rocket will launch the crewed Soyu z spacecraft for Roskosmos to the International Space Station with cosmona uts Pyotr Dubrov\, Anna Kikina and NASA astronaut Anil Menon as members of the next Expedition crew. The capsule will remain at the station for abou t six months\, providing an escape pod for the residents.\n-\nMoved forwar d from July. Delayed from June 15. LOCATION:Pad 31/6 - Baikonur Cosmodrome\, Kasachstan END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • QPS-SAR 13 DTSTART;VALUE=DATE-TIME:20260715T010000Z DTEND;VALUE=DATE-TIME:20260715T010000Z UID:228493390391 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w ill launch the QPS-SAR 13 satellite (named Mikura-I) for iQPS of Japan. R ocket Lab's mission will be named "The Grain Goddess Provides" and fly wit h an extended fairing.\n-\nQ-shu Pioneers of Space – Synthetic Aperture Radar (QPS-SAR) are operational satellites in a series of small high-resol ution SAR (synthetic aperture radar) Earth observation sats by the QPS Ins titute (iQPS). The 100kg satellites feature a 3.6m diameter antenna of onl y 10kg. It can distinguish objects 1 meter long and identify cars on the r oad. Compared to the prototypes (QPS-SAR 1\, 2)\, these satellites have in creased power due to two deployable solar arrays and increased battery cap acity. They also feature thrusters for station keeping. The planned conste llation will have 36 satellites.\n-\nDelayed from late May and June 30. Ab orted on July 1.\n\nWebcast: https://www.youtube.com/live/C_JarlUSk5I\nht tps://x.com/i/broadcasts/1nGnRRNkjROGO\nhttps://rocketlabcorp.com/live-str eam/\nhttps://www.youtube.com/live/hvSCJ2Nf754\nhttps://www.youtube.com/li ve/zKx079_ZIII\nhttps://www.youtube.com/live/5dVRL3IhJmc LOCATION:LC-1A (Rocket Lab)\, PVQ8+93\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) GSLV Mk.II • EOS 5 DTSTART;VALUE=DATE-TIME:20260715T031500Z DTEND;VALUE=DATE-TIME:20260715T071500Z UID:210712870041 DESCRIPTION:India’s Geosynchronous Satellite Launch Vehicle (GSLV)\, fly ing on the GSLV-F17 mission\, will launch the EOS 5 satellite for ISRO int o orbit. GSLV will fly in the Mk.II version with uprated HTVE engines on t he boosters and second stage\, and a CUS-15 cryogenic third stage.\n-\nEOS 5 (EOS-05 formerly known as GISAT 1A for GEO Imaging Satellite) is an Ind ian earth observing satellite operating for quick monitoring of natural ha zards and disaster. EOS 5 is built on a modified I-1K (I-1000) bus weighin g in at 2268 kg. EOS 5 carries an imaging payload consisting of of multi-s pectral (visible\, near infra-red and thermal)\, multi-resolution from 50m to 1.5km. EOS 5 will provide near real time pictures of large areas of th e country\, under cloud free conditions\, at frequent intervals. The GISAT payload consists of a 700mm Ritchey-Chretien telescope based on the Carto sat 2 design and array detectors in VNIR\, SWIR and LWIR bands\, a camera electronics and data handling system and an electronically steerable trans mit antenna system. It will operate on an orbital slot around 93.5° East for a planned service life of 7 years.\n-\nDelayed from November 2019\, Ju ly 2020\, Q1 2023\, March\, June 2024\, 2025\, Feb. 20\, Mar. 6 and May 21 . LOCATION:Second Launch Complex\, Nellore Dist\, Sriharikota\, Andhra Prade sh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Hanbit-Nano LiMER • InnoSat 0 DTSTART;VALUE=DATE:20260715 DTEND;VALUE=DATE:20260716 UID:123001187937 DESCRIPTION:An Innospace Hanbit-Nano (한빛-나노) rocket will launch on its second orbital test flight\, after a previous failure. It will launch its first proprietary test satellite\, InnoSat 0\, together with a satell ite deployer developed by South Korean space company SpaceBey. The mission will be named "?". The Korean Hanbit-Nano launcher is equipped with an el ectric turbopump powered hybrid-engine\, that uses a solid fuel (paraffin based) and liquid oxygen on the first stage\, and either a LiMER methaLOX engine or a Hyper hybrid-engine on the second stage. LOCATION:Alcântara Rocket Launch Pad A1\, Alcântara - Maranhão\, 65250- 000\, Brasilien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • Globalstar 98–106 DTSTART;VALUE=DATE:20260715 DTEND;VALUE=DATE:20260716 UID:326835750066 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch 9 new generation Globalstar communications satellites into low Earth orbit (LEO). Globalsta r M104–M112? will be the 98th to 106th satellites launched for Globalsta r's constellation. The flight is known as Globalstar 2-R Launch 1 and the Falcon 9 booster is designated as B1090.12 for this mission.\n-\nDelayed f rom May 17\, 18\, 20\, late May\, June 20 and 21.\n\nWebcast: \nhttps://ww w.spacex.com/launches/globalstar2-rlaunch1\n\nhttps://spaceflightnow.com/ LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Zhuque ZQ-3 • Test Flight DTSTART;VALUE=DATE:20260715 DTEND;VALUE=DATE:20260716 UID:563279225686 DESCRIPTION:A Landspace Zhuque ZQ-3 rocket will launch on its first test f light with a mass simulator aboard. The first stage will return for a land ing attempt. Zhuque 3 is equipped with nine TQ-12A methaLOX engines on the reusable first stage and the second stage features a TQ-15A engine optimi sed for operation in vacuum.\n-\nDelayed from April. LOCATION:LC-43/96B - Jiuquan Satellite Launch Center https://maps.app.goo. gl/wCtwtpgk3NDNoAfd6 END:VEVENT BEGIN:VEVENT SUMMARY:Busy DTSTART;VALUE=DATE-TIME:20260716T202200Z DTEND;VALUE=DATE-TIME:20260716T202200Z UID:845982359221 DESCRIPTION:Busy LOCATION: END:VEVENT BEGIN:VEVENT SUMMARY:Electron • LOXSAT 1 DTSTART;VALUE=DATE-TIME:20260717T050000Z DTEND;VALUE=DATE-TIME:20260717T050000Z UID:195119735939 DESCRIPTION:A Rocket Lab Electron rocket will launch the LOXSAT 1 mission for Eta Space &\; NASA. It is Rocket Lab's demonstration mission for t heir Photon-LEO bus\, a satellite bus based on their Photon kickstage. As proposed\, the system will be the primary payload on a Rocket Lab Photon- LEO satellite and collect critical cryogenic fluid management data in orbi t for nine months. Rocket Lab's mission will be named "?".-LOXSAT 1 is a small-scale flight demonstration of a complete cryogenic oxygen fluid man agement system developed by Eta Space and sponsored by NASA's Tipping Poin t program. After launch\, the nine-month LOXSAT 1 mission will fully demo nstrate the capability of in-space cryogenic storage and transfer. Anticip ating successful mission results\, Eta Space will use private funding to d evelop a truly commercial depot intended to serve multiple customers.-Dela yed from March\, June 2024\, February\, late 2025\, March and June 25. LOCATION:Rocket Lab Launch Complex 1\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:Long March CZ-7A • TBD DTSTART;VALUE=DATE-TIME:20260717T120000Z DTEND;VALUE=DATE-TIME:20260717T120000Z UID:855053374503 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h (Chang Zheng) CZ-7A rocket will launch an unknown payload into orbit. LOCATION:Pad 201 - Wenchang Satellite Launch Center https://goo.gl/maps/7v 4maqUT9VigBvQr5 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) HLVM3 • Gaganyaan G1 DTSTART;VALUE=DATE:20260720 DTEND;VALUE=DATE:20260721 UID:272909177671 DESCRIPTION:An Indian Human-rated Launch Vehicle Mark 3 (HLVM3) rocket wil l launch the Gaganyaan spacecraft on its first uncrewed orbital test fligh t for ISRO\, designated G1. Vyomitra\, a humanoid robot\, will be aboard G aganyaan. The mission will test the crew module in a 400km orbit\, orbital maneuvers and its reentry and recovery. The HLVM3 is the human rated vers ion of the LVM3\, which is equipped with a launch abort system (LAS) and w ill use the upgraded C32 cryo stage.\n-\nDelayed from December 2020\, Q1\, late 2021\, H2 2022\, late 2023\, December 2024\, February\, March\, June \, August\, December 2025\, January and Feb. 10. LOCATION:Second Launch Complex\, Nellore Dist\, Sriharikota\, Andhra Prade sh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • QPS-SAR 14 DTSTART;VALUE=DATE:20260720 DTEND;VALUE=DATE:20260721 UID:281832117478 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w ill launch the QPS-SAR 14 satellite (named ?) for iQPS of Japan. Rocket L ab's mission will be named "The Lightning God Defends" and fly with an ext ended fairing.\n-\nQ-shu Pioneers of Space – Synthetic Aperture Radar (Q PS-SAR) are operational satellites in a series of small high-resolution SA R (synthetic aperture radar) Earth observation sats by the QPS Institute ( iQPS). The 100kg satellites feature a 3.6m diameter antenna of only 10kg. It can distinguish objects 1 meter long and identify cars on the road. Com pared to the prototypes (QPS-SAR 1\, 2)\, these satellites have increased power due to two deployable solar arrays and increased battery capacity. T hey also feature thrusters for station keeping. The planned constellation will have 36 satellites.\n\nWebcast: \nhttps://rocketlabcorp.com/live-str eam/ LOCATION:LC-1A (Rocket Lab)\, PVQ8+93\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-3B/E • TBD DTSTART;VALUE=DATE-TIME:20260723T120000Z DTEND;VALUE=DATE-TIME:20260723T120000Z UID:572192751615 DESCRIPTION:A China Aerospace Science and Technology Corporation (CASC) Lo ng March (Chang Zheng) CZ-3B/E rocket will launch an unknown payload into orbit. LOCATION:Launch Complex 2 - Xichang Satellite Launch Center https://goo.gl /maps/jPMuSVHbzmWEYCp38 END:VEVENT BEGIN:VEVENT SUMMARY:Busy DTSTART;VALUE=DATE:20260731 DTEND;VALUE=DATE:20260801 UID:219124433245 DESCRIPTION:Busy LOCATION: END:VEVENT BEGIN:VEVENT SUMMARY:(NET) H3-24W • HTV-X2 DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:272818228776 DESCRIPTION:A Mitsubishi Heavy Industries H3 rocket will launch the second HTV-X Transfer Vehicle to the International Space Station. The HTV-X serv es as an unmanned cargo vehicle to deliver equipment and supplies to the I SS. This mission will fly the IDSS compliant JDS rendezvous and docking de monstrator (JAXA/Japan Docking System) as the sole primary external payloa d and one or more H-SSOD's (HTV-X Small Satellite Orbital Deployer). After completing its cargo delivery mission HTV-X2 will be unberthed for an aut omated docking demonstration. JAXA intends to use autonomous docking at th e lunar Gateway as well as the International Space Station.The launcher wi ll fly as 24W variant with two main engines\, four solid strap-on boosters and a wide fairing.\n-\nDelayed from H2 2024 and H1. LOCATION:Yoshinobu Launch Complex 2 - Tanegashima Space Center\, Japan\, 〒891-3703 Kagoshima\, Kumage District\, Minamitane\, Kukinaga\, 麻津 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • StriX 11 DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:303262186145 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie kickstage wil l launch the newest StriX satellite for Synspective\, its eleventh sat aft er StriX α\, β\, 1\, 3\, 4\, 2\, 5\, 6\, ? and ?. Rocket Lab's mission w ill be named "?" and will use a customized fairing.\n-\nStriX are Japanese synthetic aperture radar satellites built by Synspective for their planne d 25 satellite constellation. They feature an X-band synthetic aperture ra dar. The 100kg StriX operational satellites are more light weight than the 150kg StriX α and β prototypes. The satellites feature two deployable p anes\, one side carrying solar cells\, the other carrying the X-band radar antenna.\nSynspective is planning a constellation of 25 satellites that c an target data with a ground resolution of 1-3m\, single polarized (VV)\, and a swath width of more than 10-30km. The StriX observation modes are St ripmap and Sliding Spotlight mode and each satellite has an SAR antenna th at is 5 meters in length and stowed during launch. The simple design of th e satellites allows for affordable development of the constellation.\n\nWe bcast: \nhttps://rocketlabcorp.com/live-stream/ LOCATION:Onenui Station\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Super Heavy B3 • IFT-13 Starship B3 DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:377337508774 DESCRIPTION:A SpaceX Super Heavy rocket will launch a Starship prototype o n its 13th test flight\, designated IFT-13 (Integrated Flight Test). Stars hip will be a stretched version equipped with Raptor 3 engines and perform a payload deployment test with 22? Starlink v3 simulators and a relight o f a single Raptor engine while in space. Super Heavy will also use Raptor 3 engines and perform an ocean landing in the Gulf of Mexico. It will have an integrated vented interstage/forward dome\, three grid fins instead of the prior four\, as well as the use of the grid fins as catch points. The booster/ship combination is designated as B20/S40\, both of the Block 3 v ariant.\n-\nDelayed from mid-July.\n\nWebcast: \nhttps://www.spacex.com/la unches/starship-flight-13 LOCATION:SpaceX Starship Orbital Launch Pad\, Boca Chica Blvd\, Brownsvill e\, TX 78521\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Nuri • NeonSat & ADRSat DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:238862927992 DESCRIPTION:A Korean Nuri (KSLV-II) rocket will launch 13 satellites into orbit for Korea AeroSpace Administration (KASA) and the Korea Aerospace Re search Institute (KARI). The primary payloads are five microsatellites for the NeonSat constellation. The secondary payloads will include KARI's Sat ellite for Verifying Domestic Components No. 3 and the Active Debris Remov al Satellite (ADRSat)\, developed by the KAIST Satellite Technology Resear ch Center. Additionally 6 CubeSats will join the ride to space\, including K-STAR\, KAFASAT 2\, GIAMSat 1\, KMU ET-02 and Suncheonsat 1.\n-\nNeonSat s (New-space Earth Observation Satellite) are ~100kg Earth observation sat ellites with a high-resolution optical camera designed to monitor for natu ral disasters along the Korean Peninsula by pairing its images with artifi cial intelligence. They were developed under the NeonSat program by SaTRe C and KAIST\, Korea's leading university in science and technology.\n-\nAD RSat is equipped with robotic arms and will capture & de-orbit Korea's fir st satellite\, KitSat 1.\n-\nThe 27U CubeSat selected is KARI's 'demonstra tor for deep space exploration.' Its purpose is to conduct preliminary tra jectory research for future deep space missions by performing an orbit cha nge from Low Earth Orbit (LEO) to Geosynchronous Orbit (GSO) using low thr ust\, and to photograph the Moon and the asteroid Apophis. GSO refers to a n orbit in which a satellite circles the Earth at the same speed as the pl anet's rotation period (24 hours).\n-\nK-STAR is a 6U CubeSat from the Nat ional Security Research Institute\, which aims to test and verify national cybersecurity technologies for responding to space-based threats.\n-\nKAF ASAT 2 is a 6 u CubeSat from the Korea Air Force Academy\, intended for ca det education through the accumulation of microsatellite design and develo pment technologies.\n-\nGAIMSat 1 is a 6U CubeSat from Gwangju City\, whic h aims to secure artificial intelligence (AI) on-board data processing tec hnology and verify autonomous flight algorithms.\n-\nKMU ET-02 is a 6U Cub esat from Kookmin University\, designed for early disaster risk detection through the analysis of forest species\, vegetation\, and moisture levels nationwide\, as well as for nurturing talent in space and AI.\n-\nSuncheon sat 1 is a 3U CubeSat by Suncheon City. Its mission is to photograph the S uncheon Bay National Garden and wetlands\, analyze ecological changes\, an d verify the performance of space components from companies within the cit y.\n-\nDelayed from June. LOCATION:Second Launch Pad - Naro Space Center\, Yenae-ri\, Bongnae-myeon\ , Goheung-gun\, Jeollanam-do\, Südkorea END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • SpaceMobile 11–13 DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:279692361659 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch three BlueBird Bl ock 2 (BB2B) satellite for AST SpaceMobile. The satellites use AST & Scien ce's patented technologies for connecting to cellphones in a space environ ment for their SpaceMobile constellation. B10XX.X is the Falcon 9 booster flying this mission.\n-\nThe BlueBird Block 2 satellites are twice as larg e and have 10 times the capacity of the Block 1 sats and the BlueWalker 3  prototype. These satellites have an updated ControlSat bus\, using carbo n fiber instead of aluminium\, allowing them to be stacked and reducing th eir mass. They weigh around 4.5 tonnes each and are equipped with two sepa rate\, independent electric Xe-thruster propulsion modules. At nearly 223m ² a BB2B satellite features the largest commercial communications array i n low Earth orbit. The company needs between 45 and 60 BlueBirds for conti nuous coverage in the United States\, supporting text\, voice and data ser vices. Each satellite has a designed service life of 7 years. LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT END:VCALENDAR