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:Falcon 9 B5 • CSG 3 DTSTART;VALUE=DATE-TIME:20260103T020900Z DTEND;VALUE=DATE-TIME:20260103T020900Z UID:874058798373 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the COSMO-SkyMed Seconda Generazione 3\, or CSG 3\, radar surveillance satellite for ASI\, the Italian space agency. The mission was switched from Vega C to Falcon 9 in 2025. The Falcon 9 booster is designated as B1081.21 for this flight a nd will perform a RTLS landing at LZ-4.\n-\nCSG 3 is the third satellite o f the COSMO-SkyMed second generation (Constellation of Small Satellites fo r Mediterranean basin observation) or CSG Earth observation program of the Italian Space Agency (ASI) to replace the first generation COSMO-SkyMed s ystem. The 2230kg satellites are improved versions of the original design and utilize an enhanced version of the Prima Bus. The CSG-SAR (Synthetic A perture Radar) is a new version of the first generation X-band SAR system. The satellites will operate in the same circular sun-synchronous dawn-dus k orbit and plane as the first generation satellites with a nominal altitu de of 619km and an inclination of 97.86°.\n-\nScrubbed on Dec. 28 and 29. Delayed from Jan. 1.\n\nWebcast: https://x.com/i/broadcasts/1zqKVdlVyaYJ B\nhttps://www.spacex.com/launches/cosmo-skymedfm3\nhttps://youtu.be/6_0BD H2QK7M\nhttps://spaceflightnow.com/2025/12/27/live-coverage-spacex-to-laun ch-italian-earth-observation-satellite-on-final-falcon-9-flight-of-2025/\n https://www.youtube.com/live/Jl2UBK2Q7hc\nhttps://www.youtube.com/live/4i5 4ZGa70eE LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260104T050000Z DTEND;VALUE=DATE-TIME:20260104T050000Z UID:183229215819 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 29 Sta rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in ternally known as Starlink Group 6-88 and the booster is designated as B11 01 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mini O ptimized satellites are built by SpaceX and have a reported launch mass of 575kg. The mass-produced spacecraft carry a communications payload using the Ku and Ka frequency bands\, plus E-band for backhaul\, which will allo w Starlink to provide ~4x more capacity per satellite than earlier iterati ons. They also employ optical inter-satellite links\, phased array beam fo rming and digital processing technologies. On the v2 sats the Krypton thru sters are replaced with new and more powerful Argon Hall thrusters. The Op timized chassis features upgrades\, such as a new backhaul antenna with a SpaceX-designed and built dual-band chip and improved avionics\, propulsio n and power systems. Starlink sats are able to track on-orbit debris and c apable of autonomous collision avoidance. All satellites will be equipped with anti-reflective coatings.\nThe updated Starlink network architecture has 1584 satellites at 550km altitude and an inclination of 53 degrees\, 1 584 satellites at 540km and an inclination of 53.2 degrees\, 720 satellite s 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 44 08 Starlink satellites. Eventually SpaceX will launch and operate a follow -on network of 7518 additional Starlink satellites transmitting in V-band frequencies. In the final deployment stage an additional 30000 Starlink sa tellites might get orbited.\n-\nDelayed from Dec. 19\, 20\, 21\, 28 and Ja n. 3.\n\nWebcast: \nhttps://www.spacex.com/launches/sl-6-88\n\nhttps://sp aceflightnow.com/ LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • NeonSat 2 DTSTART;VALUE=DATE-TIME:20260105T060000Z DTEND;VALUE=DATE-TIME:20260105T080500Z UID:181303316650 DESCRIPTION:A Rocket Lab Electron rocket will launch the NeonSat 1A "verif ication satellite" for KASA\, as second satellite designed to test the cap abilities of the South Korean government's microsatellite constellation. S aTReC Initiative\, the Satellite Technology Research Center at KAIST\, an d the Korea Aerospace Research Institute (KARI) participated in the produc tion of the microsatellite. The verification satellite is intended to vali date the constellation system's technology\, identified through the first satellite in orbit. It will be placed in an afternoon orbit\, which enhanc es observation efficiency by imaging the ground at a consistent time each afternoon. It will precisely verify on-orbit thrust performance\, satellit e altitude and spacing maintenance capabilities\, and image quality. Rocke t Lab's mission will be named "Bridging The Swarm".\n-\nNeonSat 1A (New-sp ace Earth Observation Satellite) is a ~100kg Earth observation satellite w ith a high-resolution optical camera designed to monitor for natural disas ters along the Korean Peninsula by pairing its images with artificial inte lligence. It is the first satellite developed under the NeonSat program b y SaTReC and KAIST\, Korea’s leading university in science and technolog y\, which developed and operated Korea’s very first satellite KitSat 1 m ore than 30 years ago.\nThe NeonSat constellation is the first satellite s ystem developed by the Korean government using a mass-production approach for precise monitoring of the Korean Peninsula. Other NeonSats are planned to be launched in the next few years to build out the NeonSat constellat ion.\n-\nScrubbed on Dec. 11. Aborted on Dec. 16.\n\nWebcast: https://www .youtube.com/live/kBMyFpB9GPI\nhttps://x.com/i/broadcasts/1eaJbjONjbqJX\nh ttps://rocketlabcorp.com/live-stream/\nhttps://spaceflightnow.com/2025/12/ 15/rocket-lab-to-launch-second-of-three-planned-electron-rockets-this-week /\nhttps://www.youtube.com/live/ALYG_aVaKp8\nhttps://www.youtube.com/live/ zqxPpFCd4U0\nhttps://www.youtube.com/live/xSvQgPa_cww\nhttps://www.youtube .com/live/0ps2l6xy-fc LOCATION:LC-1A (Rocket Lab)\, PVQ8+93\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Pandora DTSTART;VALUE=DATE:20260105 DTEND;VALUE=DATE:20260106 UID:144375469651 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the Pandora exopl anet observatory for NASA. Pandora is a 325kg satellite designed to charac terize exoplanet atmospheres and their host stars. It is slated to observe at least 20 different planets during its one year of science operations. Another payload will be SPARCS and others ride-sharing satellites. The Fal con 9 booster is designated as B10XX.X for this flight and will perform a RTLS landing at LZ-4. LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260107T185500Z DTEND;VALUE=DATE-TIME:20260107T185500Z UID:154688890018 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 29 Sta rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in ternally known as Starlink Group 6-96 and the booster is designated as B10 69.29 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\nWebcast: \nhttps://www.spacex.com/launc hes/sl-6-96\n\nhttps://spaceflightnow.com/ LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:PSLV XL • EOS-N1 DTSTART;VALUE=DATE-TIME:20260110T041500Z DTEND;VALUE=DATE-TIME:20260110T041500Z UID:106554448576 DESCRIPTION:India’s Polar Satellite Launch Vehicle (PSLV)\, flying on th e PSLV-C62 mission in the PSLV DL configuration with two boosters\, will l aunch the EOS-N1 (Anvesha) Earth observation satellite for the DRDO. Also aboard are 18 rideshare payloads\, including the KID capsule and the SOWA 1 CubeSat.\n-\nDelayed from August 2023\, Q2\, October 2024\, Dec. 25\, 31 and Jan. 5. LOCATION:First Launch Pad\, P6MM+8V Dhawan Space Centre\, Satish\, Mobile Structure Tower\, Sriharikota\, Andhra Pradesh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • PRELUDE & OrigamiSat 2 DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:203446550525 DESCRIPTION:A Rocket Lab Electron rocket will launch 8 CubeSats for JAXA w hich were originally planned to launch together with the RAISE 4 satellite on an Epsilon S rocket. The payloads are PRELUDE\, OrigamiSat 2\, Mono-Ni kko\, ARICA 2\, Kosen 2R\, Magnaro II\, FSI-SAT 2 and Waseda-SAT 0-II. The mission was switched from Epsilon S to Electron in 2025. Rocket Lab's mis sion will be named "Kakushin Rising".\n-\nMAGNARO II are two small satelli tes developed by the Nagoya University to demonstrate formation flying tec hniques. The purpose is to develop a method to achieve resource saving\, h igh accuracy\, and formation formation by rotating and separating connecte d micro-satellites to form a formation\, and achieve simultaneous multi-po int observation and continuous Earth observation with micro-satellites. MA GNARO is launched as a 3U CubeSat sized package of 4.4kg that splits into two satellites after deployment. One is 2U and the other is 1U in size. Th ey are connected by magnetism until their separation. After separating\, t hey will maintain formation flying between 2km to 500km distance from each other. Amateur radio operators will be able to use these satellites as re peaters for long-range communication.\n-\nKOSEN 2R is a 2U CubeSat satelli te developed by a partnership between the National Institute of Technology (KOSEN)\, Yonago College\, Gunma College\, and other educational bodies. This 2.7kg satellites features a deployable Yagi-style directional antenna which extends after deployment. It is designed to study deformation of th e Earth’s crust under the sea floor. It makes use of dual reaction wheel s to maintain attitude control. It takes observations using a combination of fish-eye camera lenses and magnetic sensors.\n-\nFSI-SAT 2 is a 1U Cube sat developed by the Future Science Institute as a low cost satellite feat uring a multi-spectral camera and on-board data processing system. It is d esigned to demonstrate that this technology can be deployed and operated a t this small scale and at low cost. The satellite has a mass of only 1.4kg .\n-\nWaseda-SAT 0-II is a 1U Cubesat developed by Waseda University as a technology demonstrator for 3D-printed satellites. Its aim is to have zero fixing screws\, zero mechanical parts to be assembled together\, and zero debris. This is achieved by 3D-printing the entire chassis as a single el ement. It will be used to conduct experiments regarding deployment of memb rane surfaces which might be used as solar panels for power generation or solar sail for propulsion. The total mass of the satellite is 1.2kg. LOCATION:Onenui Station\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Zhuque ZQ-2E • TBD DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:319729239820 DESCRIPTION:A Landspace Zhuque ZQ-2E rocket will launch an unknown payload into orbit. LOCATION:LC-43/96A - Jiuquan Satellite Launch Center https://goo.gl/maps/A JroKjWe5jGVF6SV6 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) HLVM3 • Gaganyaan G1 DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:274273796178 DESCRIPTION:An Indian HLVM3 rocket will launch the Gaganyaan spacecraft on its first uncrewed orbital test flight for ISRO\, designated G1. Vyomitra \, a humanoid robot\, will be aboard Gaganyaan. The mission will test the crew module in a 400km orbit\, orbital maneuvers and its reentry and recov ery. The HLVM3 is the human rated version of the LVM3\, which is equipped with a launch abort system (LAS) and will use the upgraded C32 cryo stage. \n-\nDelayed from December 2020\, Q1\, late 2021\, H2 2022\, late 2023\, D ecember\, February\, March\, June\, August and December. LOCATION:Second Launch Complex\, Nellore Dist\, Sriharikota\, Andhra Prade sh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • Celeste 1–2 DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:127839635870 DESCRIPTION:A Rocket Lab Electron rocket will launch a pair of Celeste LEO -PNT (Low Earth Orbit Positioning\, Navigation and Timing) Pathfinder A sa tellites for ESA into a 510km low Earth orbit. Provided by European satell ite prime contractors Thales Alenia Space and GMV they will test a new app roach of providing location\, direction\, and timing services from satelli tes in low orbit and its contribution to a multi-layer navigation system. ESA's LEO-PNT demonstration mission is part of the FutureNAV program and w ill assess how a low Earth orbit fleet of satellites can work in combinati on with the Galileo and EGNOS constellations in higher orbits that provide Europe's own global navigation system. Rocket Lab's mission will be named "?".\n-\nThe two Pathfinder A satellites are large CubeSats (12U and 16U) the size of a suitcase weighing around 20kg and 30kg with payloads to bro adcast in L- and S- bands. They will validate the system definition and ea rly signal broadcast\, de-risk and demonstrate technology for the core ele ments for succeeding LEO-PNT satellites. They will operate after in-orbit commissioning for at least six months. Pathfinder B satellites are larger and more complex and will build on the knowledge acquired during the desig n\, development and integration of Pathfinder A satellites. They will carr y additional payloads to test innovative signals across frequency bands an d demonstrate the provision of additional services.\nThe Celeste 10-satell ite constellation (plus two spares) will fly in low Earth orbit to test in novative signals across various frequency bands. It is being developed und er two parallel contracts with GMV (Spain) and Thales Alenia Space (France ) as prime contractors.\n-\nDelayed from December. LOCATION:Rocket Lab Launch Complex 1\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • Starlink DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:242141323395 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 29 Sta rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in ternally known as Starlink Group 6-97 and the booster is designated as B10 XX.X for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mini Optimized satellites are built by SpaceX and have a reported launch mass of 575kg. The mass-produced spacecraft carry a communications payload usin g the Ku and Ka frequency bands\, plus E-band for backhaul\, which will al low Starlink to provide ~4x more capacity per satellite than earlier itera tions. They also employ optical inter-satellite links\, phased array beam forming and digital processing technologies. On the v2 sats the Krypton th rusters 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\, propuls ion and power systems. Starlink sats are able to track on-orbit debris and capable of autonomous collision avoidance. All satellites will be equippe d with anti-reflective coatings.\nThe updated Starlink network architectur e has 1584 satellites at 550km altitude and an inclination of 53 degrees\, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satelli tes at 570km and an inclination of 70 degrees\, and 520 satellites at 560k m and an inclination of 97.6 degrees. The initial FCC application covered 4408 Starlink satellites. Eventually SpaceX will launch and operate a foll ow-on network of 7518 additional Starlink satellites transmitting in V-ban d frequencies. In the final deployment stage an additional 30000 Starlink satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/launch es/sl-6-97\n\nhttps://spaceflightnow.com/ LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • StriX 8 DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:701305602970 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie kickstage wil l launch the newest StriX satellite for Synspective\, its eighth sat after StriX α\, β\, 1\, 3\, 4\, 2 and 5. Rocket Lab's mission will be named " Owl New World" and will use a customized fairing.\n-\nStriX are Japanese s ynthetic aperture radar satellites built by Synspective for their planned 25 satellite constellation. They feature an X-band synthetic aperture rada r. The 100kg StriX operational satellites are more light weight than the 1 50kg StriX α and β prototypes. The satellites feature two deployable pan es\, one side carrying solar cells\, the other carrying the X-band radar a ntenna.\nSynspective is planning a constellation of 25 satellites that can target data with a ground resolution of 1-3m\, single polarized (VV)\, an d a swath width of more than 10-30km. The StriX observation modes are Stri pmap and Sliding Spotlight mode and each satellite has an SAR antenna that is 5 meters in length and stowed during launch. The simple design of the satellites allows for affordable development of the constellation.\n-\nDel ayed from Q4.\n\nWebcast: \nhttps://rocketlabcorp.com/live-stream/ LOCATION:LC-1A (Rocket Lab)\, PVQ8+93\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Nebula 1 • Test Flight DTSTART;VALUE=DATE:20260110 DTEND;VALUE=DATE:20260111 UID:372532570888 DESCRIPTION:A Deep Blue Aerospace Nebula 1 (Xingyun 1) rocket will launch on its maiden flight\, which will be suborbital. The two-stage\, 3.35m dia meter launcher will use nine variable thrust\, 3D-printed Thunder-R1 (Leit ing-R) keroLOX engines on its first stage\, and a single engine on the sec ond. The first stage will be a reusable booster equipped with grid-fins a nd landing legs.\n-\nDelayed from Q2 and mid-2025. LOCATION:Hainan Commercial Launch Site END:VEVENT BEGIN:VEVENT SUMMARY:Long March CZ-3B/E • Tianlian 2-06 DTSTART;VALUE=DATE-TIME:20260115T170000Z DTEND;VALUE=DATE-TIME:20260115T170000Z UID:213920135062 DESCRIPTION:A China Aerospace Science and Technology Corporation (CASC) Lo ng March (Chang Zheng) CZ-3B/E rocket will probably launch the sixth 2nd g eneration Tianlian satellite\, Tianlian 2-06 into geosynchronous orbit. Th e 2nd gen satellites feature several technical upgrades\, including transm ission capacity and response speed. The launcher will fly as CZ-3B/G3 vari ant with a 4.2m diameter fairing.\n-\nThe Tianlian 2 (Sky Link 2) satellit es are geostationary relay satellites based on the DFH-4 bus (three-axis-s tabilized telecommunications satellite platform) with a launch mass of ~5 tonnes. Tianlian 2-06 (aka Tianlian 2F or TL-2F) will be used to support r eal-time communications between orbiting satellites and ground control sta tions. This system will replace the current network of ground-based space tracking and telemetry stations and space tracking ships. LOCATION:Launch Complex 2 - Xichang Satellite Launch Center https://goo.gl /maps/jPMuSVHbzmWEYCp38 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) GSLV Mk.II • EOS 5 DTSTART;VALUE=DATE:20260115 DTEND;VALUE=DATE:20260116 UID:182978333956 DESCRIPTION:India’s Geosynchronous Satellite Launch Vehicle (GSLV)\, fly ing on the GSLV-F18 mission\, will launch EOS 5 satellite for ISRO.\n-\nEO S 5 (EOS-05 formerly known as GISAT 1A for GEO Imaging Satellite) is an In dian earth observing satellite operating for quick monitoring of natural h azards and disaster. EOS 5 is built on a modified I-1K (I-1000) bus weighi ng in at 2268 kg. EOS 5 carries an imaging payload consisting of of multi- spectral (visible\, near infra-red and thermal)\, multi-resolution from 50 m to 1.5km. EOS 5 will provide near real time pictures of large areas of t he country\, under cloud free conditions\, at frequent intervals. The GISA T payload consists of a 700mm Ritchey-Chretien telescope based on the Cart osat 2 design and array detectors in VNIR\, SWIR and LWIR bands\, a camera electronics and data handling system and an electronically steerable tran smit 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\, J uly 2020\, Q1 2023\, March\, June 2024 and 2025. LOCATION:Second Launch Complex\, Nellore Dist\, Sriharikota\, Andhra Prade sh 524124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Agnibaan • Test Flight DTSTART;VALUE=DATE:20260115 DTEND;VALUE=DATE:20260116 UID:134947959058 DESCRIPTION:An Agnikul Agnibaan rocket will launch on its first test fligh t from the Satish Dhawan Space Centre in Sriharikota\, India. A suborbital demonstrator with only one engine\, designated SOrTeD\, launched earlier in 2024. The three stage Agnibaan rocket uses 7 electric-pump fed Agnilet keroLOX engines on the first stage\, and one vacuum-optimized Agnilet engi ne on each of the following stages.\n-\nDelayed from 2021\, 2022\, Q4 2024 and September. LOCATION:AgniKul Launch Pad - 1\, J6QP+3M\, Sriharikota\, Andhra Pradesh 5 24124\, Indien END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • SpaceMobile 7 DTSTART;VALUE=DATE:20260115 DTEND;VALUE=DATE:20260116 UID:204948854647 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the second BlueBi rd Block 2 (BB2B) satellite for AST SpaceMobile. The satellites use AST & Science's patented technologies for connecting to cellphones in a space en vironment for their SpaceMobile constellation. B10XX.X is the Falcon 9 boo ster flying this mission.\n-\nThe BlueBird Block 2 satellites are twice as large and have 10 times the capacity of the Block 1 sats and the BlueWal ker 3 prototype. The company needs between 45 and 60 BlueBirds for contin uous coverage in the United States\, supporting text\, voice and data serv ices.\n-\nDelayed from December 2024 and 2025.\n\nWebcast: \nhttps://www. spacex.com/launches LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Spectrum • Test Flight DTSTART;VALUE=DATE-TIME:20260117T200000Z DTEND;VALUE=DATE-TIME:20260117T205000Z UID:549769459319 DESCRIPTION:An Isar Aerospace Spectrum rocket will launch on its second te st flight to deploy 19 spacecraft from six institutional groups and four b usinesses across Austria\, Bulgaria\, Finland\, Germany\, Norway\, and Spa in. The mission will launch about 150kg of payload\, including satellites and their deployers\, into polar orbit. One of the payloads is FramSat 1\, another one Erminaz 1X. Spectrum is a two-stage launch vehicle propelled by liquid propane and LOX\, where stage 1 features a cluster of nine Aquil a-SL engines and stage 2 one reignitable Aquila-Vac engine.\n-\nDelayed fr om 2021\, 2022\, 2023\, August\, late 2024 and December. LOCATION:Andøya Spaceport\, Nordmelaveien\, Nordmela\, Norwegen END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Vulcan VC4S • USSF-87 DTSTART;VALUE=DATE:20260125 DTEND;VALUE=DATE:20260126 UID:203135075277 DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated ?\, will l aunch the USSF-87 mission for the US Space Force. It will carry GSSAP 7 an d 8 directly into a geosynchronous orbit. This identical pair of Geosynchr onous Space Situational Awareness satellites will form part of the USSF’ s Space Base Situational Awareness (SBSS) constellation\, which tracks spa ce traffic and debris in orbit. Vulcan will fly in the VC4S vehicle config uration with a double-engine Centaur upper stage\, four solid rocket boost ers and a standard fairing.\n-\nDelayed from late 2024\, Q1\, Q2\, August\ , September\, October and December. LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\ , FL 32780\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Pallas 1 • Test Flight DTSTART;VALUE=DATE:20260125 DTEND;VALUE=DATE:20260126 UID:305972506733 DESCRIPTION:A Galactic Energy Pallas 1 (Zhishenxing 1\, 智神星一号\, ZX-1) rocket will launch on its maiden flight to orbit. The two-stage rock et uses seven Welkin (CQ-50) keroLOX engines on the first stage and one We lkin Vac engine on the second stage. The first stage will be developed int o a reusable booster equipped with grid-fins and landing legs. Galactic En ergy (aka Xinghe Power (星河动力) or Beijing Xinghe Dongli Space Techn ology Co. Ltd.) is a Chinese launcher startup.\n-\nDelayed from November 2 024\, August\, October and December. LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf kosKTdhF5khDg8 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Nova • Test Flight DTSTART;VALUE=DATE:20260125 DTEND;VALUE=DATE:20260126 UID:300115220784 DESCRIPTION:A Stoke Space Nova rocket will launch on its maiden flight. Th e LNG/hydroLOX fueled rocket will feature a reusable first stage powered b y seven Zenith Full Flow Staged Combustion Cycle LNG engines and a second stage propelled by a revolutionary hydroLOX ring aerospike engine.\n-\nDel ayed from 2025. LOCATION:Cape Canaveral AFS Launch Complex 14\, Cape Canaveral\, Florida 3 2920\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Jielong SD-3 • PRSC DTSTART;VALUE=DATE-TIME:20260126T041300Z DTEND;VALUE=DATE-TIME:20260126T041300Z UID:592046669683 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Jielong ( Smart Dragon) SD-3 rocket will perform a sea launch from the Dongfang Hang tiangang ship near Hailing island. It will probably carry a PRSC satellite for Pakistan's SUPARCO into orbit. It seems it's a replacement for the op tical PRSS 1 launched in 2018.\n-\nDelayed from Dec. 26 and 29. LOCATION:Südchinesisches Meer END:VEVENT END:VCALENDAR