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-2C • TBD DTSTART;VALUE=DATE-TIME:20261105T160000Z DTEND;VALUE=DATE-TIME:20261105T160000Z UID:251363869332 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h (Chang Zheng) CZ-2C rocket will launch an unknown payload into orbit. LOCATION:Launch Complex 3 - Xichang Satellite Launch Center https://goo.gl /maps/DhM9rf7iHFevNapT9 END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20261106T022100Z DTEND;VALUE=DATE-TIME:20261106T022100Z UID:311530713585 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 27 Sta rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in ternally known as Starlink Group 15-21 and the booster is designated as B1 103.7 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Min i Optimized satellites are built by SpaceX and have a reported launch mass of 575kg. The mass-produced spacecraft carry a communications payload usi ng the Ku and Ka frequency bands\, plus E-band for backhaul\, which will a llow Starlink to provide ~4x more capacity per satellite than earlier iter ations. They also employ optical inter-satellite links\, phased array beam forming and digital processing technologies. On the v2 sats the Krypton t hrusters are replaced with new and more powerful Argon Hall thrusters. The Optimized chassis features upgrades\, such as a new backhaul antenna with a SpaceX-designed and built dual-band chip and improved avionics\, propul sion and power systems. Starlink sats are able to track on-orbit debris an d capable of autonomous collision avoidance. All satellites will be equipp ed with anti-reflective coatings.\nThe updated Starlink network architectu re has 1584 satellites at 550km altitude and an inclination of 53 degrees\ , 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satell ites at 570km and an inclination of 70 degrees\, and 520 satellites at 560 km and an inclination of 97.6 degrees. The initial FCC application covered 4408 Starlink satellites. Eventually SpaceX will launch and operate a fol low-on network of 7518 additional Starlink satellites transmitting in V-ba nd frequencies. In the final deployment stage an additional 30000 Starlink satellites might get orbited.\n-\nDelayed from Nov. 1 and 5.\n\nWebcast:  \nhttps://www.spacex.com/launches/sl-15-21\n\nhttps://spaceflightnow.com / LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:Ceres 2 • TBD DTSTART;VALUE=DATE-TIME:20261106T233800Z DTEND;VALUE=DATE-TIME:20261106T233800Z UID:229985796262 DESCRIPTION:A Galactic Energy Ceres 2 (Gushenxing 2\, GX-2) rocket will la unch on its second flight. The three stage solid-fueled Ceres 2 rocket is topped with a liquid-fueled upper stage.\n-\nDelayed from Nov. 4. LOCATION:LC-43/95A - Jiuquan Satellite Launch Center https://goo.gl/maps/p bNBUb1duneU9V2n6 END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • USSF-432 DTSTART;VALUE=DATE-TIME:20261107T004600Z DTEND;VALUE=DATE-TIME:20261107T004600Z UID:267118467159 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the USSF-432 miss ion (previously designated R-4) for the U.S. Space Force. Payload is proba bly a stack of 23 Starshield satellites. The mission likely is the 6th of 18 for the USSF's Space Based Sensing and Targeting (SBST) portfolio\, whi ch includes the Space Data Network (SDN) Backbone and the Space-Based Airb orne Moving Target Indicator (SB-AMTI) program. The Falcon 9 booster is B1 095.8 for this flight.\n-\nDelayed from Nov. 3 and 4.\n\nWebcast: \nhttps ://www.spacex.com/launches/ussf432\n\nhttps://spaceflightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:Long March CZ-12 • Guowang DTSTART;VALUE=DATE-TIME:20261108T211700Z DTEND;VALUE=DATE-TIME:20261108T211700Z UID:284745083122 DESCRIPTION:A Shanghai Academy of Spaceflight Technology (SAST) Long Marc h (Chang Zheng) CZ-12 rocket will launch a batch of 9 Hulianwang Digui sat ellites for the China SatNet Guowang internet constellation into orbit. Gu owang satellites either use the mega-constellation's small satellite platf orm\, weighing about 695kg each\, or a large satellite platform\, around 3 0% bigger and weighing up to 1 tonne. Both platforms utilize electric prop ulsion systems to maneuver in orbit\, powered by two solar panels. This mi ssion is known as SatNet LEO Group 29 (卫星互联网低轨29组) and the satellites are designated as Hulianwang Digui 29A/B/C/D/E/F/G/H/I\, built on the small platform.\n-\nThe Guowang satellite program can carry a vari ety of payloads\, including broadband communication payloads\, laser commu nication payloads\, synthetic aperture radar payloads\, optical remote sen sing payloads\, and others\, to meet the needs of different users and scen arios. It offers comprehensive technical support across numerous fields su ch as maritime and aviation operations\, information security\, navigation and positioning\, and meteorological research\, while also enabling expan sion into the global satellite internet access market. The eventual conste llation is expected to grow to 12992 satellites. This will be made up of 6 080 in the low orbit GW-A59 sub-constellation at altitudes below 500km\, o ffering initial broadband coverage. The rest will orbit in the higher GW-A 2 sub-constellation at 1145km\, providing a more global reach.\n-\nDelayed from Nov. 6. LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf kosKTdhF5khDg8 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Super Heavy/Starship B3 • TBD DTSTART;VALUE=DATE:20261108 DTEND;VALUE=DATE:20261109 UID:235123228184 DESCRIPTION:A SpaceX Super Heavy rocket will launch a Starship prototype o n its 15th and second? orbital flight\, designated IFT-15 (Integrated Flig ht Test). Starship is equipped with upgraded Raptor 3 engines and will per form an orbit insertion burn\, fly at an altitude approximately 275 km abo ve Earth and complete approximately six orbits around the planet over the course of a nearly 10-hour flight\, including a payload deployment of 26? Starlink V3 satellites followed by deorbit burn\, for a catch attempt at t he launch tower. Super Heavy will also perform a catch attempt at the towe r. The booster/ship combination is designated as B22/S42\, both of the Blo ck 3 variant.\n\nStatic fire: https://www.youtube.com/live/BlyqwOjCJzA\nht tps://www.youtube.com/live/t8RZHIfgQ3A\nhttps://x.com/i/broadcasts/1MJgNbR jlryGL\n-\nStarlink v3 satellites are built by SpaceX and have a reported launch mass of ~2 tonnes. The mass-produced spacecraft carry a communicati ons payload using the Ku and Ka frequency bands\, plus E-band for backhaul \, which will allow Starlink to provide ~10x more capacity per satellite t han earlier iterations. They also employ optical inter-satellite links\, p hased array beam forming and digital processing technologies. Like the v2 satellites the v3 sats are equipped with more powerful Argon Hall thruster s. Starlink sats are able to track on-orbit debris and capable of autonomo us collision avoidance. All satellites will be equipped with anti-reflecti ve coatings.\nThe updated Starlink network architecture has 1584 satellite s at 550km altitude and an inclination of 53 degrees\, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satellites at 570km and an inclination of 70 degrees\, and 520 satellites at 560km and an inclination of 97.6 degrees. The initial FCC application covered 4408 Starlink satell ites. Eventually SpaceX will launch and operate a follow-on network of 751 8 additional Starlink satellites transmitting in V-band frequencies. In th e final deployment stage an additional 30000 Starlink satellites might get orbited.\n-\nDelayed from late October.\n\nWebcast: \nhttps://www.spacex. com/launches/starship-flight-15\nhttps://spaceflightnow.com/ LOCATION:Starship Orbital Launch Pad 2\, 54018 TX-4\, Brownsville\, TX 785 21\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • R-5 DTSTART;VALUE=DATE-TIME:20261110T030300Z DTEND;VALUE=DATE-TIME:20261110T030300Z UID:170328098163 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the USSF-? missio n (previously designated R-5) for the U.S. Space Force. Payload is probabl y a stack of 23 Starshield satellites. The mission likely is the 7th of 18 for the USSF's Space Based Sensing and Targeting (SBST) portfolio\, which includes the Space Data Network (SDN) Backbone and the Space-Based Airbor ne Moving Target Indicator (SB-AMTI) program. The Falcon 9 booster is B10X X.X for this flight.\n\nWebcast: \nhttps://www.spacex.com/launches/ussf43 2\n\nhttps://spaceflightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Kinetica 1 • TBD DTSTART;VALUE=DATE:20261110 DTEND;VALUE=DATE:20261111 UID:286871118105 DESCRIPTION:A CAS Space Kinetica 1 (Lijian 1) rocket will launch a collect ion of eight satellites into orbit. LOCATION:LC-43/130 - Jiuquan Satellite Launch Center https://goo.gl/maps/w gnZZd2mnu5jbriLA END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • R-6 DTSTART;VALUE=DATE-TIME:20261113T042300Z DTEND;VALUE=DATE-TIME:20261113T042300Z UID:173962249503 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the USSF-? missio n (previously designated R-6) for the U.S. Space Force. Payload is probabl y a stack of 23 Starshield satellites. The mission likely is the 8th of 18 for the USSF's Space Based Sensing and Targeting (SBST) portfolio\, which includes the Space Data Network (SDN) Backbone and the Space-Based Airbor ne Moving Target Indicator (SB-AMTI) program. The Falcon 9 booster is B10X X.X for this flight.\n\nWebcast: \nhttps://www.spacex.com/launches/ussf43 2\n\nhttps://spaceflightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:Vulcan VC6L • Amazon Leo DTSTART;VALUE=DATE-TIME:20261113T233000Z DTEND;VALUE=DATE-TIME:20261113T233000Z UID:186878318551 DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated V-004?\, w ill launch a batch of 40 operational satellites for Amazon's Kuiper conste llation. The mission is known as Vulcan Leo 1 by ULA and LV-01 by Amazon. The Centaur stage will deploy the satellites in an initial orbit of 450km altitude\, the satellites will then use their electric propulsion systems to settle into their assigned final orbits. The Kuiper constellation will enable Internet service for customers between 56 degrees north and south l atitude. Vulcan will fly in the VC6L vehicle configuration with a double-e ngine Centaur CV-L upper stage\, six solid rocket boosters and a long fair ing. CV-L\, is 1.94m shorter than the original Centaur V\, now renamed CV- HE (Centaur V High Energy). Unlike the CV-HE\, which uses a hydrolox-fuele d reaction control system\, the CV-L will employ a hydrazine-fueled RCS.\n -\nOperational satellites of the Amazon Leo constellation (formerly known as Project Kuiper) are a significant upgrade from the two prototype satell ites of the Kuiper Protoflight mission. The ~572kg satellites are equipped with Hall-effect thruster technology for propulsion. They feature improve d systems and sub-systems on board\, including phased array antennas\, pro cessors\, solar arrays\, propulsion systems\, and optical inter-satellite links. In addition\, the satellites are coated in a dielectric mirror film unique to Amazon Leo that scatters reflected sunlight to help make them l ess visible to ground-based astronomers. Amazon Leo is planned to work in concert with Amazon's network of 12 satellite ground station facilities. I n addition to connecting to ground stations\, satellites will interconnect via optical infrared laser connections. Amazon refers to this technology as OISL (optical inter-satellite link).\nThe Amazon Leo constellation is p lanned to consist of 3236 satellites operating in 98 orbital planes in t hree orbital shells\, one each at 590km\, 610km and 630km orbital altitud e. Kuiper satellites will fly in mid-inclination orbits\, enabling Interne t service for customers between 56 degrees north and south latitude. Phase 1 of deployment will be 578 satellites at 630km altitude and an orbital i nclination of 51.9 degrees. A total of five phases of constellation develo pment are planned.\n-\nDelayed from September\, December 2025\, Q1\, Augus t\, September and October.\n\nWebcast:\nhttps://www.ulalaunch.com/missions /next-launch/vulcan-leo-1 LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\ , FL 32780\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • QPS-SAR 19 DTSTART;VALUE=DATE:20261114 DTEND;VALUE=DATE:20261115 UID:336617256164 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w ill launch the QPS-SAR 19 satellite (named Yamatsumi-II) for iQPS of Japan . Rocket Lab's mission will be named "The Mountain God Rises" 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 radar Earth observation sats by the QPS Institute (iQPS). The 100kg satellites feature a 3.6m diameter antenna of only 10kg. It can distinguis h objects 1 meter long and identify cars on the road. Compared to the prot otypes (QPS-SAR 1\, 2)\, these satellites have increased power due to two deployable solar arrays and increased battery capacity. They also feature thrusters for station keeping. The full constellation will have 36 satelli tes.\n-\nDelayed from Nov. 10.\n\nWebcast: \nhttps://rocketlabcorp.com/li ve-stream/ LOCATION:Onenui Station\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • NROL-195 DTSTART;VALUE=DATE-TIME:20261115T223400Z DTEND;VALUE=DATE-TIME:20261115T223400Z UID:738197598902 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the classified NR OL-195 mission for the National Reconnaissance Office. It is for the first phase of NRO's imaging satellite constellation built by SpaceX and Northr op Grumman and is understood to be the 15th of multiple batches to launch. The NRO's Proliferated Architecture is a constellation of intelligence sa tellites\, including imaging and relay satellites. The 9? satellites on th is launch are built upon SpaceX' Starshield bus\, with Northrop Grumman pr oviding sensors for some of them. The booster is designated B1XXX.X for th is mission and will perform a RTLS landing at LZ-4.\n-\nDelayed from Nov. 5.\n\nWebcast: \nhttps://www.spacex.com/launches/nrol195\n\nhttps://space flightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) PSLV CA • TDS 1 DTSTART;VALUE=DATE:20261115 DTEND;VALUE=DATE:20261116 UID:397873564509 DESCRIPTION:ISRO's Polar Satellite Launch Vehicle (PSLV)\, flying on the P SLV-63 mission in the PSLV CA configuration without boosters\, will launch the Technology Demonstration Satellite 1 (TDS 1) into orbit.\n-\nTDS 1 (T DS-01) is supposed to host demonstrators for an electric propulsion system \, an indigenous atomic clock\, Travelling Wave Tube Amplifier (TWTA) and Quantum Key Distribution.\n-\nDelayed from late March 2022\, March\, Octob er\, late 2024\, Q2 and late October. LOCATION:Satish Dhawan Space Centre\, Sriharikota\, Andhra Pradesh 524124\ , Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) HLVM3 • Gaganyaan G1 DTSTART;VALUE=DATE:20261115 DTEND;VALUE=DATE:20261116 UID:147371642923 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\, Feb. 10 and August. LOCATION:Second Launchpad\, P69J+W5X\, Sriharikota\, Shar Project\, Andhra Pradesh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • TBD DTSTART;VALUE=DATE:20261115 DTEND;VALUE=DATE:20261116 UID:234944319340 DESCRIPTION:A Rocket Lab Electron rocket topped with a modified upper stag e will launch on a HASTE (Hypersonic Accelerator Suborbital Test Electron) suborbital mission\, designated "?"\, for an unknown customer (probably Anduril). LOCATION:LC2\, 41 N Seawall Rd\, Wallops Island\, VA 23337\, Vereinigte St aaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-8A • Guowang DTSTART;VALUE=DATE-TIME:20261120T120000Z DTEND;VALUE=DATE-TIME:20261120T120000Z UID:116513350529 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h (Chang Zheng) CZ-8A rocket will launch a batch of 9 Hulianwang Digui sat ellites for the China SatNet Guowang internet constellation into orbit. Gu owang satellites either use the mega-constellation's small satellite platf orm\, weighing about 695kg each\, or a large satellite platform\, around 3 0% bigger and weighing up to 1 tonne. Both platforms utilize electric prop ulsion systems to maneuver in orbit\, powered by two solar panels. This mi ssion is known as SatNet LEO Group 30 (卫星互联网低轨30组) and the satellites are designated as Xingwang Digui 30A/B/C/D/E/F/G/H/I\, and wer e built on the small platform.\n-\nThe Guowang satellite program can carry a variety of payloads\, including broadband communication payloads\, lase r communication payloads\, synthetic aperture radar payloads\, optical rem ote sensing payloads\, and others\, to meet the needs of different users a nd scenarios. It offers comprehensive technical support across numerous fi elds such as maritime and aviation operations\, information security\, nav igation and positioning\, and meteorological research\, while also enablin g expansion into the global satellite internet access market. The eventual constellation is expected to grow to 12992 satellites. This will be made up of 6080 in the low orbit GW-A59 sub-constellation at altitudes below 50 0km\, offering initial broadband coverage. The rest will orbit in the high er GW-A2 sub-constellation at 1145 km\, providing a more global reach. LOCATION:Pad 1 - Hainan Commercial Launch Site https://maps.app.goo.gl/2na KfJxVaF8UG7J59 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Ariane 64 B2 • Amazon Leo DTSTART;VALUE=DATE:20261123 DTEND;VALUE=DATE:20261124 UID:402738462200 DESCRIPTION:Arianespace will launch an Ariane 6 rocket\, on a flight desig nated VA271\, to put a batch of 36 operational satellites for the Amazon L eo constellation into orbit. The mission is known as LE-03 by Amazon. Aria ne 6 will fly in the Ariane 64 Block 2 configuration\, using four P160C ro cket boosters and a long fairing.\n-\nOperational satellites of the Amazon Leo constellation (formerly known as Project Kuiper) are a significant up grade from the two prototype satellites of the Kuiper Protoflight mission. The ~572kg satellites are equipped with Hall-effect thruster technology f or propulsion. They feature improved systems and sub-systems on board\, in cluding phased array antennas\, processors\, solar arrays\, propulsion sys tems\, and optical inter-satellite links. In addition\, the satellites are coated in a dielectric mirror film unique to Amazon Leo that scatters ref lected sunlight to help make them less visible to ground-based astronomers . Amazon Leo is planned to work in concert with Amazon's network of 12 sat ellite ground station facilities. In addition to connecting to ground stat ions\, satellites will interconnect via optical infrared laser connections . Amazon refers to this technology as OISL (optical inter-satellite link). \nThe Amazon Leo constellation is planned to consist of 3236 satellites op erating in 98 orbital planes in three orbital shells\, one each at 590k m\, 610km and 630km orbital altitude. Kuiper satellites will fly in mid-in clination orbits\, enabling Internet service for customers between 56 degr ees north and south latitude. Phase 1 of deployment will be 578 satellites at 630km altitude and an orbital inclination of 51.9 degrees. A total of five phases of constellation development are planned.\n-\nDelayed from Oct . 7.\n\nWebcast:\nhttps://www.arianespace.com/road-to-space/ LOCATION:ELA4 (l'Ensemble de Lancement Ariane 6) - Centre Spatial Guyanais \, Französisch-Guyana END:VEVENT BEGIN:VEVENT SUMMARY:Soyuz 2.1b • Progress MS-36 / ISS 97P DTSTART;VALUE=DATE-TIME:20261124T050300Z DTEND;VALUE=DATE-TIME:20261124T050300Z UID:120623827313 DESCRIPTION:A RKTs Progress Soyuz 2.1b rocket will launch the 97th Progre ss cargo delivery ship for Roskosmos to the International Space Station.\n -\nDelayed from Aug. 17 and Sep. 9. LOCATION:Pad 31/6 - Baikonur Cosmodrome\, Kasachstan END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-12 • Guowang DTSTART;VALUE=DATE-TIME:20261124T080000Z DTEND;VALUE=DATE-TIME:20261124T080000Z UID:327861273587 DESCRIPTION:A Shanghai Academy of Spaceflight Technology (SAST) Long Marc h (Chang Zheng) CZ-12 rocket will launch a batch of 9 Hulianwang Digui sat ellites for the China SatNet Guowang internet constellation into orbit. Gu owang satellites either use the mega-constellation's small satellite platf orm\, weighing about 695kg each\, or a large satellite platform\, around 3 0% bigger and weighing up to 1 tonne. Both platforms utilize electric prop ulsion systems to maneuver in orbit\, powered by two solar panels. This mi ssion is known as SatNet LEO Group 31 (卫星互联网低轨31组) and the satellites are designated as Hulianwang Digui 31A/B/C/D/E/F/G/H/I\, built on the small platform.\n-\nThe Guowang satellite program can carry a vari ety of payloads\, including broadband communication payloads\, laser commu nication payloads\, synthetic aperture radar payloads\, optical remote sen sing payloads\, and others\, to meet the needs of different users and scen arios. It offers comprehensive technical support across numerous fields su ch as maritime and aviation operations\, information security\, navigation and positioning\, and meteorological research\, while also enabling expan sion into the global satellite internet access market. The eventual conste llation is expected to grow to 12992 satellites. This will be made up of 6 080 in the low orbit GW-A59 sub-constellation at altitudes below 500km\, o ffering initial broadband coverage. The rest will orbit in the higher GW-A 2 sub-constellation at 1145km\, providing a more global reach. LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf kosKTdhF5khDg8 END:VEVENT BEGIN:VEVENT SUMMARY:Long March CZ-2F/G • Shenzhou 24 DTSTART;VALUE=DATE-TIME:20261125T001000Z DTEND;VALUE=DATE-TIME:20261125T001000Z UID:235841144264 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h 2F/G rocket will launch the Shenzhou 24 spacecraft\, a crewed mission to dock with the orbiting China space station CSS. Ye Guangfu (叶光富)?\, ? and a Pakistani astronaut (Muhammad Zeeshan Ali or Khurram Daud) will l aunch on China's latest crewed space mission.\n-\nDelayed from late Octobe r. LOCATION:LC-43/91 (Pad 921 / South Launch Site 1) - Jiuquan Satellite Laun ch Center https://goo.gl/maps/7v4maqUT9VigBvQr5 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • Globalstar DTSTART;VALUE=DATE:20261125 DTEND;VALUE=DATE:20261126 UID:250974949140 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch 9 new generation Globalstar communications satellites (designated as HIBLEO-4) into low Ear th orbit (LEO). Globalstar M11?–M11? will be the 106th to 114th satellit es launched for Globalstar's constellation. Globalstar reserves 85% of its network capacity for Apple’s Emergency SOS via Satellite service. The s eventeen 500kg satellites under this contract\, built by MDA with Lightnin g buses supplied by Rocket Lab\, are intended to sustain and grow that cap acity through the middle of the next decade. Each satellite is also expect ed to support Globalstar’s broader Band 53 terrestrial-spectrum services . The flight is known as Globalstar 2-R Launch 2 and the Falcon 9 booster is designated as B10XX.X for this mission and will perform a RTLS landing at LZ-40. The second stage will fly with a shortened nozzle and a reused f airing.\n-\nDelayed from late October.\n\nWebcast: \nhttps://www.spacex.co m/launches/globalstar2-rlaunch2\n\nhttps://spaceflightnow.com/ LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Spectrum • AT-Astra & GreenBox 2 DTSTART;VALUE=DATE-TIME:20261126T200000Z DTEND;VALUE=DATE-TIME:20261126T200000Z UID:326690852713 DESCRIPTION:An Isar Aerospace Spectrum rocket will launch on its third fli ght to carry two GreenBox satellites for the Austrian company R-Space into orbit. GreenBox 1 is named AT-Astra (aka IOB-01) and represents the first com­mer­cial sa­tel­lite fully developed and built in Austria. It is a platform for IOD (in-orbit demonstration) for experiments from three cus tomers\; Austrian companies Enpulsion and SunBooster\, and the Portuguese firm Synopsis Planet. The mission will be named "?" by Isar and "R-Space I OD-1" by the customer. Spectrum is a two-stage launch vehicle propelled by liquid propane and LOX\, where stage 1 features a cluster of nine Aquila- SL engines and stage 2 one reignitable Aquila-Vac engine.\n-\nAT-Astra\, a 2U CubeSat\, is the first com­mer­cial sa­tel­lite fully developed an d built in Austria and will carry experiments from three customers. ENPULS ION is one of the world's leading providers of electric propulsion systems based on Field Emission Electric Propulsion (FEEP) technology. On AT-Astr a it supports the OOBI project (On-Orbit Behaviour of Indium)\, heating sa mples of indium\, the propellant used in its FEEP thrusters\, to their mel ting point to observe how liquid metal behaves in microgravity\, with imag es downlinked via the R-Space Greenbox platform. SunBooster is a Graz-base d company testing a newly developed solar module in orbit for the first ti me. Its design combines surface-mount (SMT) micro solar cells with mini bl ocking diodes to improve resilience against micrometeorites while keeping costs low\, targeting a tenfold cost reduction compared with existing spac e solar modules. Synopsis Planet features a compact\, high-performance sta r tracker that combines precise attitude determination and space-debris de tection in a single unit. Developed with the University of Lisbon and fund ed by PRR New Space Portugal\, it processes data on board for real-time st ar identification and moving-object detection\, simplifying spacecraft arc hitecture and reducing downlink needs. LOCATION:Andøya Spaceport\, Nordmelaveien\, Nordmela\, Norwegen END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • NG-25 Cygnus XL CRS2 DTSTART;VALUE=DATE-TIME:20261129T160000Z DTEND;VALUE=DATE-TIME:20261129T160000Z UID:158264562369 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch with the latest C ygnus XL cargo freighter on an operational cargo delivery flight to the In ternational Space Station. Total cargo mass is ?kg\, including ... The mis sion is known as NG-25 and the spacecraft is named SS James A. Lovell\, wh ich will fly for the second phase of the commercial resupply services (CRS ) contract for NASA. The mission was switched from Antares 330 to Falcon m id-2025. The booster is designated B10XX.X for this mission and will perfo rm a RTLS landing at LZ-40.\n\nWebcast: \nhttps://www.spacex.com/launches /ng25 LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Yuanxingzhe 1 • Test Flight DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:576728611128 DESCRIPTION:A Space Epoch (SEPOCH) Yuanxingzhe 1 (Voyager 1\, 元行者一 号) rocket will launch on its first test flight\, after a successful subo rbital hop and water landing earlier in 2025. Yuanxingzhe 1 is a two-stage \, liquid-fueled\, partially reusable rocket powered by Longyun-70 (Dragon Cloud) restartable methaLOX engines. The first stage of the rocket is ex pected to land vertically on a sea based platform using landing legs.\n-\n Delayed from December 2025. LOCATION:TBD END:VEVENT BEGIN:VEVENT SUMMARY:(NET) LVM3 • Mangalyaan 2 DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:256353535710 DESCRIPTION:An Indian Launch Vehicle Mark 3 (LVM3) rocket will launch the Mangalyaan 2 (Mars Orbiter Mission 2\, MOM 2) on an Earth-escape trajector y to investigate the planet Mars.\n-\nDelayed from late 2024. LOCATION:Second Launch Complex\, Nellore Dist\, Sriharikota\, Andhra Prade sh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Kinetica 2 • Qianfan DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:734062764800 DESCRIPTION:A CAS Space Kinetica 2 rocket will launch on its third? flight \, to put a batch of 18 satellites for the Qianfan Xingzuo (千帆星座\, "Thousand Sails"\, formerly known as G60) internet constellation of Shang hai Spacecom Satellite Technology (SSST)\, a Chinese equivalent of SpaceX ’s Starlink satellites. The sats are designated as Qianfan ?A–?R for t he Qianfan Group ?. Each Qianfan satellite is believed to weigh 300kg in a flat pack design\, with a single solar array\, to fit as many satellites as possible inside the rocket fairing in two parallel stacks. For maneuver ing in orbit\, each satellite has an electric hall-effect thruster burning krypton to generate 20 millinewtons of thrust\, with a specific impulse o f 1385 seconds. The initial tranche will use 1296 satellites. Ultimately\, the Spacesail constellation will consist of more than 14000 low-orbit bro adband multimedia satellites. Kinetica 2 (Lijian 2) was developed by CAS Space (a.k.a. Beijing Zhongke Aerospace Exploration Technology Co.)\, a sp in-off of the Chinese Academy of Sciences. It is equipped with 3 YF-102 ke roLOX engines on its first stage and side boosters and will be developed i nto reusability. LOCATION:LC-43/140 - Jiuquan Satellite Launch Center https://maps.app.goo. gl/C5QccUL9HvRGr9629 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon Heavy • GM1 CLPS DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:273398433974 DESCRIPTION:A SpaceX Falcon Heavy rocket will launch the 6360kg Griffin lu nar lander for Voyager Technologies (previously Astrobotic)\, as part of N ASA's CLPS lunar program (CLPS 20A). Griffin Mission 1 (GM1) will land nea r the lunar south pole at Mons Mouton and Nobile crater. Main payload will be Astrolab's FLIP (FLEX Lunar Innovation Platform) rover which will carr y a NASA laser retroflector. Aboard the lander is also Voyager's own BEACO N CubeRover\, European Space Agency's LandCam-X landing-camera system and Nanofiche GLPH (Galactic Library to Preserve Humanity)\, a tiny archive of human history\, to the moon's surface. NASA's VIPER rover was removed fro m this mission. This Falcon Heavy flight will feature side boosters B10XX. X and B11XX.X\, which will return for a RTLS landing at LZ-2 and LZ-40\, p lus center core B1099.\n-\nDelayed from November 2024\, December 2025 and November. LOCATION:Launch Pad 39A\, Cape Canaveral\, Florida 32920\, Vereinigte Staa ten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Vega C • IRIDE DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:146822477914 DESCRIPTION:An Avio Vega C rocket\, designated VV31?\, will launch the sec ond batch of IRIDE Earth observation satellites for The Italian Space Agen cy ASI and ESA. The 11 satellites on this flight are designated IRIDE-HYP- PLATINO 1–2\, IRIDE-MS1-EAGLET2 11\, IRIDE-SAR-NIMBUS 1–6\, IRIDE-SAR- NOX 1 and IRIDE-VHR-NIMBUS 1. IRIDE is a space-based observation program initiated under the framework of Italy's National Recovery and Resilience Plan (PNRR). IRIDE will be unique in its incorporation of a wide range of sensing techniques and technologies\, including microwave imaging with Syn thetic Aperture Radars (SAR)\, optical imaging at high and medium resoluti ons\, and coverage across panchromatic\, multispectral\, hyperspectral\, a nd infrared bands. Once operational\, IRIDE will be used to track the impa cts of climate change and provide data to support startups and SMEs in cre ating commercial applications. Also aboard this launch are a number of Pro méthée satellites for the Japetus constellation.\n-\nDelayed from Octobe r 1\, Q4 2025 and June. LOCATION:ELV\, 66PG+C22\, Carbet Toukan 97310\, Französisch-Guyana END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Vulcan VC6L • Amazon Leo DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:148320414083 DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated V00?\, wil l launch a batch of 40 operational satellites for Amazon's Kuiper constell ation. The mission is known as Amazon Leo ? by ULA and LV-02 by Amazon. Th e Centaur stage will deploy the satellites in an initial orbit of 450km al titude\, the satellites will then use their electric propulsion systems to settle into their assigned final orbits. The Kuiper constellation will en able Internet service for customers between 56 degrees north and south lat itude. Vulcan will fly in the VC6L vehicle configuration with a double-eng ine Centaur CV-L upper stage\, six solid rocket boosters and a long fairin g. CV-L\, is 1.94m shorter than the original Centaur V\, now renamed CV-HE (Centaur V High Energy). Unlike the CV-HE\, which uses a hydrolox-fueled reaction control system\, the CV-L will employ a hydrazine-fueled RCS.\n-\ nOperational satellites of the Amazon Leo constellation (formerly known as Project Kuiper) are a significant upgrade from the two prototype satellit es of the Kuiper Protoflight mission. The ~572kg satellites are equipped w ith Hall-effect thruster technology for propulsion. They feature improved systems and sub-systems on board\, including phased array antennas\, proce ssors\, solar arrays\, propulsion systems\, and optical inter-satellite li nks. In addition\, the satellites are coated in a dielectric mirror film u nique to Amazon Leo that scatters reflected sunlight to help make them les s visible to ground-based astronomers. Amazon Leo is planned to work in co ncert with Amazon's network of 12 satellite ground station facilities. In addition to connecting to ground stations\, satellites will interconnect v ia optical infrared laser connections. Amazon refers to this technology as OISL (optical inter-satellite link).The Amazon Leo constellation is plann ed to consist of 3236 satellites operating in 98 orbital planes in three  orbital shells\, one each at 590km\, 610km and 630km orbital altitude. K uiper satellites will fly in mid-inclination orbits\, enabling Internet se rvice for customers between 56 degrees north and south latitude. Phase 1 o f deployment will be 578 satellites at 630km altitude and an orbital incli nation of 51.9 degrees. A total of five phases of constellation developmen t are planned. LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\ , FL 32780\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Kinetica 1 • TBD DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:491332826609 DESCRIPTION:A CAS Space Kinetica 1 (Lijian 1) rocket will launch a collect ion of nine satellites into orbit. LOCATION:LC-43/130 - Jiuquan Satellite Launch Center https://goo.gl/maps/w gnZZd2mnu5jbriLA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) LVM3 • GSAT 32 DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:116829939620 DESCRIPTION:ISRO’s Launch Vehicle Mark 3 (LVM3) rocket\, flying on the L VM3-M? mission\, will launch the GSAT 32 (GSAT-N3) communications satellit e for ISRO (Indian Space Research Organization). GSAT 32 will replace the dead-on-arrival GSAT 6A satellite\, which launched in April 2018. The miss ion was switched from GSLV to LVM3 in 2025.\n-\nDelayed from October 2019\ , February\, August 2020\, 2022\, late 2024\, mid-2025 and Q2. LOCATION:Satish Dhawan Space Centre\, Sriharikota\, Andhra Pradesh 524124\ , Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-10B • Guowang DTSTART;VALUE=DATE:20261201 DTEND;VALUE=DATE:20261202 UID:774556281670 DESCRIPTION:A China Rocket (CALT) Long March (Chang Zheng) CZ-10B rocket will launch on its second flight\, with a batch of 18 GuoWang (国网) sat ellites for China Satellite Network Group (中国卫星网络集团有限 公司). The CZ-10B first stage is powered by seven YF-100N keroLOX engine s\, the second stage is propelled by a YF-219 methaLOX engine. The first s tage is reusable and will attempt a landing? on the drone ship Linghangzhe (领航者)\, via its tension wires recovery system on its deck. LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf kosKTdhF5khDg8 END:VEVENT END:VCALENDAR