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 • PWSA 71–91 DTSTART;VALUE=DATE-TIME:20260716T203200Z DTEND;VALUE=DATE-TIME:20260716T203200Z UID:307327178945 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch 21 operational s atellites for the U.S. military’s Space Development Agency PWSA (Prolife rated Warfighter Space Architecture) constellation. The Tranche 1 satellit es (codenamed Praetorian) on this flight are for the Transport Layer and w ere built by York Space. The mission is designated as SDA-T1TL-E and the F alcon 9 booster is B1103.4 for this flight. The 2nd stage is equipped with a Mission Extension Kit. Comprising a gray band on the RP-1 tank\, extra helium bottles & batteries\, this kit extends the life of the stage in-orb it\, allowing it to deploy the payload directly into its operational orbit .\n-\nOnce fully operational\, the SDA Transport Layer will consist of a p roliferated heterogeneous constellation of data relay space vehicles (SVs) that provide persistent global coverage through a mesh network comprised of communication satellites that connect to one another and to other space vehicles and ground stations via optical intersatellite links (OISLs). By nature of the mesh network spanning the globe\, the Transport satellites will also be able to transmit precise position\, navigation and timing (PN T) data to enhance GPS. A-class satellites have at least four optical cros s-links\, that is so they can talk to satellites that are in plane with on e another as they're traveling and they also can talk to satellites that a re cross-plane or in completely different orbits. So they can maintain tho se four lines of communication simultaneously. The B-class satellites will connect directly to the warfighters via the Link-16 military communicatio ns system. They have two optical cross-links each\, so that allows them to maintain constant communication with the other transport satellites in pl ane. The two other nodes will be Link-16 transmitters. Link-16 is an exist ing tactical communication system used across the services primarily for a ir and ground systems to share low latency data. The first phase of SDA’ s Proliferated Warfighter Space Architecture consists of 28 satellites (Tr anche 0 including 20 communications payloads made by Lockheed Martin and Y ork Space\, and eight missile-tracking infrared sensor satellites made by SpaceX and Leidos) as a proof of concept for the missile tracking and data relay network\, followed by more than 150 additional satellites to provid e an initial operational capability. In total\, Tranche 1 will consist of 154 operational satellites: 126 in the transport layer developed by York\, Northrop Grumman\, and Lockheed Martin\, and 28 focused on missile warnin g and tracking developed by Northrop Grumman and L3Harris. Combining conve ntional tactical radio links\, laser inter-satellite communications\, and wide-view infrared sensors\, hundreds more SDA spacecraft could launch lat er as the Pentagon ramps up efforts and integrates new capabilities.\n-\nD elayed from Q1 2024\, Q2\, Q4 2025 and Q1.\n\nWebcast: https://x.com/i/bro adcasts/1kJzDDmBBArKv\nhttps://www.spacex.com/launches/sda-t1tl-e\nhttps:/ /www.youtube.com/live/rLAfNp2CtrY\nhttps://spaceflightnow.com/2026/07/16/l ive-coverage-spacex-to-launch-21-communications-satellites-for-the-space-d evelopment-agency/\nhttps://www.youtube.com/live/M0agOywbDIU\nhttps://www. youtube.com/live/ufOqrUfRKFU\nhttps://www.youtube.com/live/_FfgWWmIZUw LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Soyuz 2.1b • Rassvet DTSTART;VALUE=DATE-TIME:20260716T090000Z DTEND;VALUE=DATE-TIME:20260716T205900Z UID:301972725365 DESCRIPTION:A RKTs Progress Soyuz 2 rocket will launch a batch of 16 sate llites for the Buro 1440's Rassvet project\, a planned low-orbit communica tions constellation. These satellites will be part of the Rassvet-3 sub-co nstellation and will operate in orbits with an inclination of 82.3°. The other two constellations (Rassvet 1 and 2) will have inclinations of 60° and 88° respectively. Initially ~288 sats will provide global coverage\, scaling to 730+ and later up to 1000. They operate in LEO at 500-800km alt itude\, use Ku/Ka bands\, and are equipped with laser inter-links. The roc ket will fly in the Soyuz 2.1b configuration with a 81KS type fairing.\n-\ nDelayed from June. LOCATION:Pad 43/4 - Plesetsk Cosmodrome https://goo.gl/maps/kQduw6ZJdtw3nC nk6 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Soyuz 2.1b • GLONASS 148 DTSTART;VALUE=DATE-TIME:20260716T090000Z DTEND;VALUE=DATE-TIME:20260716T210000Z UID:333806383629 DESCRIPTION:A Roscosmos Soyuz rocket will launch the latest GLONASS-K navi gation satellite\, designated GLONASS-K1 №19L\, into medium Earth orbit (MEO). The spacecraft is the 6th Uragan-K to be launched\, and overall the 148th spacecraft of the GLONASS program. The rocket will fly in the Soyuz 2.1b configuration with a Fregat-M upper stage.\n-\nGLONASS-K (Uragan-K) spacecraft are the third generation of GLONASS navigation satellites. The Uragan-K1 satellites have an increased lifetime of 10–12 years\, reduced weight of only 935kg and offer an additional L-Band navigational signal. The payload consists of L-Band navigation signals in 25 channels separated by 0.5625 MHz intervals in two frequency bands: 1602.5625 - 1615.5 MHz an d 1240 - 1260 MHz. EIRP 25 to 27 dBW. Right hand circular polarized. On-bo ard cesium clocks provide time accuracy to 1000 nanoseconds. A civil refer ence signal on L2 frequency is to be added after the completion of flight testing of Glonass-M in 2004 to substantially increase the accuracy of nav igation relaying on civil signals. A third civil reference signal within t he new frequency band of 1164-1215 MHz offered by the Glonass-K1 satellite enables civil airlines to use satellite-aided positioning as the primary navigation facility. The new Uragan-K1 spacecraft also carries instrumenta tion of the KOSPAS-SARSAT international search-and-rescue system.\nGLONASS (Globalnaya Navigationnaya Sputnikovaya Sistema\, Global Orbiting Navigat ion Satellite System) is a Russian space-based navigation system comparabl e to the American GPS system\, which consists of Uragan spacecraft. The op erational system contains 21 satellites in 3 orbital planes\, with 3 on-or bit spares. GLONASS provides 100 meters accuracy with its C/A (deliberatel y degraded) signals and 10–20 meter accuracy with its P (military) signa ls. LOCATION:Pad 43/3 - Plesetsk Cosmodrome https://goo.gl/maps/GX9Jpfr5hGdhG2 t8A END:VEVENT BEGIN:VEVENT SUMMARY:Super Heavy B3 • IFT-13 Starship B3 DTSTART;VALUE=DATE-TIME:20260716T224500Z DTEND;VALUE=DATE-TIME:20260717T001500Z UID:254271153679 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 20 Starlink v3 satellites and a relight of a single Raptor engine while in space. The Starlinks will extend solar ar rays and antennas and will attempt to connect with ground stations in Sout h Africa and the larger Starlink constellation via high-capacity lasers. T he Starlink satellites will be on the same suborbital trajectory as Starsh ip. Six of the satellites have been modified with a suite of cameras to sc an Starship’s heat shield and transmit imagery down to operators to cont inue testing methods of analyzing Starship’s heat shield readiness for R TLS on future missions. Several tiles on Starship have been painted white to simulate missing tiles and serve as imaging targets in the test. Super Heavy will also use Raptor 3 engines and perform an ocean landing in the G ulf 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 gri d fins as catch points. The booster/ship combination is designated as B20/ S40\, both of the Block 3 variant.\n\nLive pad view: https://www.youtube.c om/live/mhJRzQsLZGg\nhttps://www.youtube.com/live/tolIxDZYBHs\n\nWebcast: https://x.com/i/broadcasts/1MKgNNXAZdmxL\nhttps://www.spacex.com/launches/ starship-flight-13\nhttps://www.youtube.com/live/WXHd014xLjQ\nhttps://spac eflightnow.com/2026/07/16/live-coverage-spacex-to-deploy-first-starlink-v3 -satellites-on-suborbital-starship-super-heavy-flight/\nhttps://www.youtub e.com/live/dZ6-A4iZFWU\nhttps://www.youtube.com/live/ubVe02oNDww\nhttps:// www.youtube.com/live/beKsuJUsiWk\nhttps://www.youtube.com/live/TtzECiryPXw \nhttps://www.youtube.com/live/2r31rEkUUaA\nhttps://x.com/i/broadcasts/1OG wbbYrlzRKB LOCATION:SpaceX Starship Orbital Launch Pad\, Boca Chica Blvd\, Brownsvill e\, TX 78521\, Vereinigte Staaten 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:Vikram I • Solaras S3 & Scope DTSTART;VALUE=DATE-TIME:20260718T050000Z DTEND;VALUE=DATE-TIME:20260718T090000Z UID:279370046723 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\, February and July 12.\n\nWe bcast: https://youtube.com/@skyrootaerospaceofficial 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:(NET) Electron • QPS-SAR 13 DTSTART;VALUE=DATE-TIME:20260720T010000Z DTEND;VALUE=DATE-TIME:20260720T010000Z UID:206324700416 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:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260720T140000Z DTEND;VALUE=DATE-TIME:20260720T140000Z UID:265396807391 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 17-39 and the booster is designated as B 1082.23 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 18.\n\nWebcast: \n https://www.spacex.com/launches/sl-17-39\n\nhttps://spaceflightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Hanbit-Nano LiMER • InnoSat 0 DTSTART;VALUE=DATE:20260720 DTEND;VALUE=DATE:20260721 UID:892820286380 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:20260720 DTEND;VALUE=DATE:20260721 UID:190351392728 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:Falcon 9 B5 • MRV-MEP DTSTART;VALUE=DATE-TIME:20260721T211500Z DTEND;VALUE=DATE-TIME:20260722T011500Z UID:142535149361 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the MRV (Mission Robotic Vehicle) satellite servicer for Northrop Grumman into GTO\, develo ped for DARPA's RSGS (Robotic Servicing of Geosynchronous Satellites) prog ram. The 3 tonne MRV was built by the Northrop Grumman-owned company Space Logistics. It is designed to attach up to 30 MEPs (Mission Extension Pods) to satellites in GEO over the course of its life. MEPs (Mission Extension Pods) are 400kg spacecraft designed to be captured by the MRV and then at tached to a customer's satellite. A single MEP can extend a 2 tonne satell ite's service life by up to 6 years. 2 of the MEPs on this flight will ser vice satellites for Intelsat\, while the third will service a satellite fo r Optus. The Falcon 9 booster is designated as B1069.32 for this mission a nd will be expended\, so it's flying without recovery hardware.\n\nWebcast : \nhttps://www.spacex.com/launches/\n\nhttps://spaceflightnow.com/ LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate n END:VEVENT BEGIN:VEVENT SUMMARY:Gravity YL-1 • Dongpo 13–14/17–20 & Fengxing 1 DTSTART;VALUE=DATE-TIME:20260722T025200Z DTEND;VALUE=DATE-TIME:20260722T025200Z UID:298049964176 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 East China Sea n ear Shanghai. Payloads are the Dongpo 13 –14 and 17–20 satellites of t he "Ring Constellation".  This constellation currently has 14 satellites in orbit. The six satellites to be launched this time include two optical satellites and four SAR satellites\, representing iterative upgrades in pe rformance and comprehensive complementarity of payload advantages. Another payload will be Fengxing 1 (锋行一号). Gravity 1 (引力一号 or Yin li 1) is an all solid rocket with four boosters\, which will be capable of land and sea launches. For liftoff only the boosters ignite\, with the co re stage getting lit shortly before booster separation.\n-\nDelayed from N ovember 2024\, December 2025 and June 10. LOCATION:Ostchinesisches Meer END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-3B/E • TBD DTSTART;VALUE=DATE-TIME:20260723T110000Z DTEND;VALUE=DATE-TIME:20260723T110000Z UID:197899511963 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:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260724T140000Z DTEND;VALUE=DATE-TIME:20260724T140000Z UID:258516909698 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 17-51 and the booster is designated as B 1081.26 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 23.\n\nWebcast: \n https://www.spacex.com/launches/sl-17-51\n\nhttps://spaceflightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) GSLV Mk.II • EOS 5 DTSTART;VALUE=DATE-TIME:20260725T031500Z DTEND;VALUE=DATE-TIME:20260725T071500Z UID:315643094798 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) Electron • QPS-SAR 14 DTSTART;VALUE=DATE:20260725 DTEND;VALUE=DATE:20260726 UID:818792250154 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:Long March CZ-8A • Guowang DTSTART;VALUE=DATE-TIME:20260727T120000Z DTEND;VALUE=DATE-TIME:20260727T120000Z UID:119387663209 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. Th is mission is known as SatNet LEO Group 23 (卫星互联网低轨23组) an d the satellites are designated as Xingwang Digui 23A/B/C/D/E/F/G/H/I.\n-\ nThe Guowang satellite program can carry a variety of payloads\, including broadband communication payloads\, laser communication payloads\, synthet ic aperture radar payloads\, optical remote sensing payloads\, and others\ , to meet the needs of different users and scenarios. It offers comprehens ive technical support across numerous fields such as maritime and aviation operations\, information security\, navigation and positioning\, and mete orological research\, while also enabling expansion into the global satell ite 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 500km\, offering initial broadband c overage. The rest will orbit in the higher 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:Long March CZ-7A • TBD DTSTART;VALUE=DATE-TIME:20260729T115000Z DTEND;VALUE=DATE-TIME:20260729T115000Z UID:250715813490 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h (Chang Zheng) CZ-7A rocket will launch an unknown payload into orbit.\n- \nDelayed from July 17. LOCATION:Pad 201 - Wenchang Satellite Launch Center https://goo.gl/maps/7v 4maqUT9VigBvQr5 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) 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 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) 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) HLVM3 • Gaganyaan G1 DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:335605657997 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) Zhuque ZQ-3 • Test Flight DTSTART;VALUE=DATE:20260801 DTEND;VALUE=DATE:20260802 UID:933775442796 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:(NET) Spectrum • Platform 6 & TRISAT-S DTSTART;VALUE=DATE-TIME:20260806T200000Z DTEND;VALUE=DATE-TIME:20260806T213500Z UID:269001007059 DESCRIPTION:An Isar Aerospace Spectrum rocket will launch on its second te st flight to carry 5 CubeSats and one non-separable payload into orbit. Th e payloads are Platform 6\, TriSat-S\, SpaceTeamSat 1\, FramSat 1\, CyBEEs at and Let It Go (Dcubed\, non-separable experiment). The mission will be named "Onward And Upward". Spectrum is a two-stage launch vehicle propelle d by liquid propane and LOX\, where stage 1 features a cluster of nine Aqu ila-SL engines and stage 2 one reignitable Aquila-Vac engine.\n-\nThe Endu roSat 6U CubeSat Platform 6 is a fully integrated microsatellite capable o f supporting up-to 4U (7.5kg) payloads.\n-\nTRISAT-S is a scientific and e ducational 3U CubeSat mission led by the University of Maribor in cooperat ion with Slovenian company SkyLabs. The primary objective of the TRISAT-S mission is to demonstrate two critical technology domains for future long- duration and deep-space exploration: advanced battery hibernation performa nce and ultra-miniaturized imaging-based navigation. It has a launch mass of 5kg.\n-\nSpaceTeamSat 1 is a CubeSat project of the TU Wien Space Team using a 1U CubeSat to serve as a live laboratory in space. The mission is a complement to the CanSat Challenge (ESERO Austria)\, where students of A HS and BHS can perform their own experiments on the CubeSat. For this purp ose\, various sensors as well as cameras are on board the satellite.\n-\nF ramSat 1 is a 1.3kg 1U CubeSat to test a sun sensor made by Eidel. The sat ellite was manufactured by Orbit NTNU.\n-\nCyBEEsat is a technology demons tration mission by the TU Berlin to demonstrate a miniaturized transceiver for the Short Duration Mission (SDM) frequency band and cybersecurity app lications. The 1U CubeSat satellite features innovative on-board hardware as well as radiation tolerant perovskite solar cells.\n-\nDelayed from 202 1\, 2022\, 2023\, August\, late 2024 and December. Scrubbed on Jan. 21. De layed from Mar. 19 and 23. Aborted on Mar. 25. Delayed from Mar. 28. Scrub bed on Apr. 9. Delayed from mid-May. Scrubbed on June 15.\n\nWebcast: http s://www.youtube.com/live/Ss1DUqLjecc\nhttps://www.youtube.com/live/uUc2d_N PBN0\nhttps://www.youtube.com/live/EIb7Q0W5MuQ\nhttps://www.youtube.com/li ve/8STqoxAWMJY LOCATION:Andøya Spaceport\, Nordmelaveien\, Nordmela\, Norwegen END:VEVENT BEGIN:VEVENT SUMMARY:(NET) RFA One B1 • Test Flight DTSTART;VALUE=DATE-TIME:20260810T150000Z DTEND;VALUE=DATE-TIME:20260810T190000Z UID:200317160794 DESCRIPTION:Rocket Factory Augsburg will launch a RFA One Block 1 rocket o n its maiden flight from the SaxaVord Spaceport on the Shetland Islands. I t will fly a research mission for Ukraine-based Lunar Research Service (LR S) and the PocketQubes ERMINAZ 1U\, ERMINAZ 1V\, MARIA-G (HADES-F)\, QUBIK 5 and UNNE 1 (HADES-E). Seven companies had been selected by DLR to launc h payloads aboard the maiden RFA flight\, totaling 136kg. The companies se lected were TU Munich\, SPACEMIND\, Planetary Transportations Systems\, AM SAT-Deutschland\, DCUBED\, and Kinetik Space. The three stage launcher is powered by nine keroLOX Helix engines on the first stage and one Helix eng ine on the second stage. The third stage (named RFA Redshift) is powered b y a nitromethane and N2O consuming Fenix engine\, and will also be used as OTV. Eventually the first stage will be developed into the Block 2 varian t and reused by parachute-assisted ocean recovery on later flights.\n-\nDe layed from late 2022\, March\, July\, December 2023\, May\, August 2024\, summer and late 2025. LOCATION:SaxaVord Spaceport\, Unst\, Shetland ZE2 9EF\, Vereinigtes König reich END:VEVENT END:VCALENDAR