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BEGIN:VEVENT
SUMMARY:(NET) Zhuque ZQ-2E B2 • Xingshidai
DTSTART;VALUE=DATE:20261014
DTEND;VALUE=DATE:20261015
UID:168128029185
DESCRIPTION:A Landspace Zhuque ZQ-2E Block 2 rocket will launch a batch of
  8 satellites for the Taikong Jisuan "Space Computing Constellation" into 
 orbit. The Xingshidai satellites from ADA Space are for testing in-orbit d
 ata processing capabilities with artificial intelligence assistance\, as w
 ell as inter-satellite laser link communication techniques. The satellites
  form their own network using laser links that operate at up to 100 gigabi
 ts per second. They are equipped with the company’s self-developed AI te
 chnology\, which utilizes up to eight billion parameters\, and remote sens
 ing payloads. This initial constellation can process five peta operations 
 per second (POPS). The company plans to launch 2800 satellites and increas
 e processing to 1000 POPS.
LOCATION:LC-43/96A - Jiuquan Satellite Launch Center https://goo.gl/maps/A
 JroKjWe5jGVF6SV6
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • USSF-481
DTSTART;VALUE=DATE-TIME:20261015T234400Z
DTEND;VALUE=DATE-TIME:20261015T234400Z
UID:255836341266
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the USSF-481 miss
 ion (previously designated TH-2) for the U.S. Space Force. Payload is prob
 ably a stack of 17 Starshield satellites. The mission likely is the 5th of
  18 for the USSF's Space Based Sensing and Targeting (SBST) portfolio\, wh
 ich includes the Space Data Network (SDN) Backbone and the Space-Based Air
 borne Moving Target Indicator (SB-AMTI) program. The Falcon 9 booster is B
 1081.28 for this flight.
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Kinetica 2 • Qianfan
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:384068879656
DESCRIPTION:A CAS Space Kinetica 2 rocket will launch on its second? fligh
 t\, to put a batch of 18 satellites for the Qianfan Xingzuo (千帆星座\
 , "Thousand Sails"\, formerly known as G60) internet constellation of Shan
 ghai 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.\n-\nDelayed from September.
LOCATION:LC-43/140 - Jiuquan Satellite Launch Center https://maps.app.goo.
 gl/C5QccUL9HvRGr9629
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Kuaizhou KZ-11 • DEAR 6 & DEAR 11
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:854371216679
DESCRIPTION:An ExPace Kuaizhou (Clipper) KZ-11 rocket will launch the DEAR
  6 (B300-L03) and DEAR 11 (B300-F01) recoverable capsule for AZSpace as o
 ne payload stack into into a near-Earth circular orbit at an altitude of 3
 60km and an inclination of 41.5°. Both capsules are connected by a node m
 odule and resemble an uncrewed mini space station. The DEAR (Discovery Exp
 loration Advance Recovery) B300 complex will test technologies for uncrewe
 d spacecraft\, including rendezvous and docking tests and reentry and retu
 rn tests in orbit. DEAR 11 will return to Earth after operating independen
 tly in orbit for about a month.\n-\nDelayed from August.
LOCATION:LC-43/95B - Jiuquan Satellite Launch Center
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Ceres 1S • TBD
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:242282309268
DESCRIPTION:A Galactic Energy Ceres 1S rocket will perform a sea launch fr
 om Haiyang Spaceport\, where it will lift off from the DeFu 15001 barge (
 德浮15001号)?\, carrying an unknown payload into orbit. The mission is 
 named "The Sea Facing the City of Rams". Ceres 1 will fly as 1S variant (S
  for sea launch\, aka Gushenxing 1H (GX-1H) for haiyang = ocean) which has
  a different thrust profile\, with reduced thrust on the first stage and i
 ncreased thrust on the following stages.
LOCATION:Gelbes Meer
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • Bandwagon-5
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:770122567578
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch on the Bandwagon-
 5 rideshare mission with ? satellites to a mid-inclination orbit. The boos
 ter is designated B10XX.X for this mission and will perform a RTLS landing
  at LZ-2?.\n\nWebcast: \nhttps://www.spacex.com/launches/bandwagon-5\n\nht
 tps://spaceflightnow.com/
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate
 n
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Gravity YL-2 • Test Flight
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:278040962904
DESCRIPTION:An Orienspace Gravity 2 rocket will perform its first flight.
  Gravity 2 (引力二号 or Yinli 2) is equipped with a recoverable first
  stage propelled by nine Yuanli-110 (Force-110) keroLOX engines and a seco
 nds stage using one Yuanli-110 vacuum optimized engine. The first stage is
  equipped with gridfins & landing legs and can be enhanced with expendable
  solid boosters.\n-\nDelayed from December\, September 2025 and mid-2026.
LOCATION:Hainan Commercial Launch Site
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Kinetica 1 • TBD
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:265114560164
DESCRIPTION:A A CAS Space Kinetica 1 (Lijian 1) rocket will perform its f
 irst sea launch from Haiyang Spaceport\, where it will lift off from the D
 ongfang Hangtiangang (东方航天港号) ship\, carrying a collection of 
 nine satellites into orbit.
LOCATION:Gelbes Meer
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Spectrum • Greenbox 1–2
DTSTART;VALUE=DATE:20261015
DTEND;VALUE=DATE:20261016
UID:411992218053
DESCRIPTION:An Isar Aerospace Spectrum rocket will launch on its third? fl
 ight to carry Greenbox 1 and 2 for R-Space into orbit. The mission will be
  named "?" by Isar and "R-Space IOD-1" by the customer. Spectrum is a two-
 stage launch vehicle propelled by liquid propane and LOX\, where stage 1 f
 eatures a cluster of nine Aquila-SL engines and stage 2 one reignitable Aq
 uila-Vac engine.
LOCATION:Andøya Spaceport\, Nordmelaveien\, Nordmela\, Norwegen
END:VEVENT
BEGIN:VEVENT
SUMMARY:H3-24L • MMX & Idefix
DTSTART;VALUE=DATE-TIME:20261019T194100Z
DTEND;VALUE=DATE-TIME:20261019T194100Z
UID:821261648529
DESCRIPTION:A Mitsubishi Heavy Industries H3 rocket will launch the Martia
 n Moon Explorer mission MMX. The flight is designated as H3F10. After spen
 ding a year in transit\, the MMX spacecraft will enter orbit around Mars\,
  where the exploration module will begin mapping and characterizing the su
 rfaces of Phobos and Deimos using its eight scientific instruments. When t
 he spacecraft makes a close pass to Phobos\, between 40 and 100 meters fro
 m the surface\, it will deploy the Idefix rover\, which will then spend th
 e next three months studying targets of interest\, including sites where t
 he MMX spacecraft will gather samples for analysis on Earth. The launcher 
 will fly as 24L variant with two main engines\, four solid strap-on booste
 rs and a long fairing.\n-\nThe MMX spacecraft consists of three modules: t
 he propulsion\, the exploration\, and the sample return capsule. The explo
 ration module has landing legs and a suite of instruments\, including a Ga
 mma ray and Neutron Spectrometer (MEGANE) provided by NASA\, a Wide Angle 
 Multiband Camera (WAM)\, a Near-Infrared Spectrometer (MacrOmega) provided
  by CNES\, a Telescopic Camera (TL)\, a Light Detection and Ranging (LIDAR
 ) instrument\, the Circum-Martian Dust Monitor (CMDM) and a Mass Spectrum 
 Analyzer (MSA). The xploration module will also carry and deploy the Idef
 ix rover. The exploration module and sample return capsule are connected t
 o the propulsion module\, where the thrusters and propellant tanks are loc
 ated.\n-\nDelayed from August and September 2024.
LOCATION:Yoshinobu Launch Complex 2 - Tanegashima Space Center\, Japan\, 
 〒891-3703 Kagoshima\, Kumage District\, Minamitane\, Kukinaga\, 麻津
END:VEVENT
BEGIN:VEVENT
SUMMARY:GSLV Mk.II • NavIC 12
DTSTART;VALUE=DATE:20261020
DTEND;VALUE=DATE:20261021
UID:334186586152
DESCRIPTION:India’s Geosynchronous Satellite Launch Vehicle (GSLV)\, fly
 ing on the GSLV-F1? mission\, will launch the NVS 3 navigation satellite f
 or ISRO. It is the third next generation satellite in the fleet and will r
 eplace the failed NVS 2 satellite in the Indian Regional Navigation Satell
 ite System NavIC\, which aims to improve positioning services over India a
 nd neighboring regions. It will be positioned at 111.75º East\, to replac
 e IRNSS 1E. GSLV will fly in the Mk.II version with uprated HTVE engines o
 n the boosters and second stage\, and a CUS-15 cryogenic third stage.\n-\n
 NVS 3 (NVS-03) is the twelfth satellite in the Navigation with Indian Cons
 tellation (NavIC) and the third 2nd generation NavIC satellite. This new s
 eries of satellites have a launch mass of 2250kg\, incorporate L1 band sig
 nals additionally to L5 and S-band and use indigenous atomic clocks. The s
 atellite is powered by two solar arrays\, which generate up to 1660 Watts\
 , and has a lifetime of 12 years.\nThree of the satellites in the NavIC co
 nstellation are in GEO (Geostationary Orbit) at 32.5°\, 83° and 131.5° 
 East\, while four satellites are in an inclined geosynchronous orbit with 
 an inclination of 29° with longitude crossing at 55° and 111.75° East. 
 All satellites are inter-operable and compatible with GPS and Galileo.\n-\
 nDelayed from December and Oct. 13.
LOCATION:Second Launchpad\, P69J+W5X\, Sriharikota\, Shar Project\, Andhra
  Pradesh 524124\, Indien
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • Blacksky 25
DTSTART;VALUE=DATE:20261020
DTEND;VALUE=DATE:20261021
UID:324974441912
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch the sixth BlackSky Gen 3 satellite (designated Global 35?)  int
 o a circular 470km orbit. Rocket Lab's mission is named "?".\n-\nThe Black
 Sky constellation of 1m resolution Earth observation microsatellites will 
 be deployed by BlackSky Global LLC. The Gen 3 satellite's enhanced capabil
 ities include short-wave infrared sensors that can penetrate smoke and haz
 e\, as well as the ability to conduct multiple observations of the same lo
 cation within a day. The satellite’s inter-satellite laser links will en
 able rapid retasking for time-sensitive missions\, a feature particularly 
 valuable for defense and intelligence applications.\n-\nDelayed from Septe
 mber.\n\nWebcast: \nhttps://rocketlabcorp.com/live-stream/
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Tianlong TL-3 • Test Flight
DTSTART;VALUE=DATE:20261020
DTEND;VALUE=DATE:20261021
UID:156894018935
DESCRIPTION:A Space Pioneer Tianlong 3 rocket will launch on its second fl
 ight. The two stage launcher is powered by nine Tianhuo TH-12 keroLOX engi
 nes on the first stage and a staged combustion cycle keroLOX engine on the
  2nd stage. Tianlong 3 is planned to feature a reusable first stage on lat
 er flights.\n-\nDelayed from September and late 2024.
LOCATION:LC-43/120B - Jiuquan Satellite Launch Center
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • HawkEye
DTSTART;VALUE=DATE:20261020
DTEND;VALUE=DATE:20261021
UID:788410266554
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch a batch of two small radio frequency monitoring satellites into
  orbit for RF geospatial analytics provider Hawkeye 360. The mission is na
 med "?".\n-\nHawk 16A/B are 30kg? satellites based on the Defiant bus by H
 awkEye 360 and are part of a space-based civil global intelligence network
  that will use radio frequency (RF) technology to help monitor transportat
 ion across air\, land and sea and assist with emergencies\, which is essen
 tially a civil SIGINT (Signal Intelligence) mission. The constellation of 
 small satellites\, called HawkEye\, in low Earth orbit (LEO) will collect 
 information on specific radio signals worldwide to provide high-precision 
 radio frequency mapping and analytics.\n\n-\nDelayed from September.
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Ariane 64 B2 • Amazon Leo
DTSTART;VALUE=DATE:20261020
DTEND;VALUE=DATE:20261021
UID:242557034710
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:(NET) Long March CZ-8A • Guowang
DTSTART;VALUE=DATE-TIME:20261022T030000Z
DTEND;VALUE=DATE-TIME:20261022T030000Z
UID:194588004819
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 28 (卫星互联网低轨28组) and the
  satellites are designated as Xingwang Digui 28A/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) SSLV • AayulSAT 1A & CubeSat
DTSTART;VALUE=DATE:20261025
DTEND;VALUE=DATE:20261026
UID:157870449837
DESCRIPTION:A NewSpace India Limited (NSIL) SSLV rocket will launch on its
  first operational flight\, designated SSLV-L1\, to place AayulSAT 1A and 
 the CubeSat PARIKSHIT into orbit.\n-\nThe 25kg AayulSAT 1A is a reflight o
 f the mini-tanker satellite by OrbitAID to demonstrate on-orbit internal p
 ropellant transfer\, power transfer\, and data transfer using their patent
 ed Standard Interface for Docking and Refueling Port (SIDRP).\n-\nDelayed 
 from Q4 2024 and 2025.
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) Alpha B2 • ConnectedCosmos 3–8
DTSTART;VALUE=DATE:20261025
DTEND;VALUE=DATE:20261026
UID:249118488858
DESCRIPTION:A Firefly Aerospace Alpha Block 2 rocket will launch on a flig
 ht designated FLTA008?\, to put six satellites for the ConnectedCosmos sov
 ereign LEO constellation\, operated by Open Cosmos\, into orbit. The Conne
 ctedCosmos constellation is designed to provide independent and resilient 
 connectivity infrastructure for Europe and the world using high-priority K
 a-band spectrum filings by the Principality of Liechtenstein. Firefly name
 d the mission "?". The new Block 2 upgrade of Alpha features stretched and
  strengthened propellant tanks with improved insulation as well as upgrade
 d avionics.\n-\nDelayed from September.
LOCATION:Vandenberg AFB Space Launch Complex 2\, Tangair Rd\, Lompoc\, CA 
 93437\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • Globalstar
DTSTART;VALUE=DATE:20261029
DTEND;VALUE=DATE:20261030
UID:617741295752
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\nWebcast: \nhttps://www.spacex.com/launches/globalstar2-rlaunch2
 \n\nhttps://spaceflightnow.com/
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate
 n
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC6L • Amazon Leo
DTSTART;VALUE=DATE:20261029
DTEND;VALUE=DATE:20261030
UID:304785364132
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated V00?\, wil
 l launch a batch of 42 operational satellites for Amazon's Kuiper constell
 ation. The mission is known as Amazon Leo ? by ULA and LV-01 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.\n-\nDelayed from September\, December 2025\, Q1\, August an
 d September.
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:20261101
DTEND;VALUE=DATE:20261102
UID:228804781639
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:(NET) PSLV CA • TDS 1
DTSTART;VALUE=DATE:20261101
DTEND;VALUE=DATE:20261102
UID:240709603584
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) Falcon Heavy • GM1 CLPS
DTSTART;VALUE=DATE:20261101
DTEND;VALUE=DATE:20261102
UID:196375962787
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. Aboard the lan
 der is also Voyager's own BEACON CubeRover\, European Space Agency's LandC
 am-X landing-camera system and a NASA laser retroflector. NASA's VIPER rov
 er was removed from this mission. This Falcon Heavy flight will feature si
 de boosters B10XX.X and B11XX.X\, which will return for a RTLS landing at 
 LZ-2 and LZ-40\, plus center core B1099.\n-\nDelayed from November 2024 an
 d December 2025.
LOCATION:Launch Pad 39A\, Cape Canaveral\, Florida 32920\, Vereinigte Staa
 ten
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) HLVM3 • Gaganyaan G1
DTSTART;VALUE=DATE:20261101
DTEND;VALUE=DATE:20261102
UID:131820401752
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) 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 Raptor 3 engines and will perform an o
 rbit insertion burn\, fly at an altitude approximately 275 km above 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 splashdown near the coast o
 f Chile. Super Heavy will perform an ocean landing in the Gulf of Mexico. 
 It will have an integrated vented interstage/forward dome\, three grid fin
 s instead of the prior four\, as well as the use of the grid fins as catch
  points. The booster/ship combination is designated as B22/S42\, both of t
 he Block 3 variant.\n-\nStarlink v3 satellites are built by SpaceX and hav
 e a reported launch mass of ~2 tonnes. The mass-produced spacecraft carry 
 a communications payload using the Ku and Ka frequency bands\, plus E-band
  for backhaul\, which will allow Starlink to provide ~10x more capacity pe
 r satellite than earlier iterations. They also employ optical inter-satell
 ite links\, phased array beam forming and digital processing technologies.
  Like the v2 satellites the v3 sats are equipped with more powerful Argon 
 Hall thrusters. Starlink sats are able to track on-orbit debris and capabl
 e of autonomous collision avoidance. All satellites will be equipped with 
 anti-reflective coatings.\nThe updated Starlink network architecture has 1
 584 satellites at 550km altitude and an inclination of 53 degrees\, 1584 s
 atellites 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 a
 n inclination of 97.6 degrees. The initial FCC application covered 4408 St
 arlink satellites. Eventually SpaceX will launch and operate a follow-on n
 etwork of 7518 additional Starlink satellites transmitting in V-band frequ
 encies. In the final deployment stage an additional 30000 Starlink satelli
 tes 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
END:VCALENDAR