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BEGIN:VEVENT
SUMMARY:Electron • HawkEye 47–49
DTSTART;VALUE=DATE-TIME:20261023T071100Z
DTEND;VALUE=DATE-TIME:20261023T071100Z
UID:234978409080
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 "We're Not Hawking Around".\n-\nHawk 16A/B/C are 30kg satellites based
  on the Defiant bus by HawkEye 360 and are part of a space-based civil glo
 bal intelligence network that will use radio frequency (RF) technology to 
 help monitor transportation across air\, land and sea and assist with emer
 gencies\, which is essentially a civil SIGINT (Signal Intelligence) missio
 n. The constellation of small satellites\, called HawkEye\, in low Earth o
 rbit (LEO) will collect information on specific radio signals worldwide to
  provide high-precision radio frequency mapping and analytics.\n-\nDelayed
  from September. Scrubbed on Oct. 21.\n\nWebcast: https://www.youtube.com/
 live/LddRNoiKJ7U\nhttps://rocketlabcorp.com/live-stream/\nhttps://www.yout
 ube.com/live/UyT0Lp2ZPls\nhttps://www.youtube.com/live/sJrSRKgCGFw\nhttps:
 //www.youtube.com/live/aYuC6EOExsM
LOCATION:LC-1A (Rocket Lab)\, PVQ8+93\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:Long March CZ-6A • Yaogan 50-03
DTSTART;VALUE=DATE-TIME:20261023T101500Z
DTEND;VALUE=DATE-TIME:20261023T101500Z
UID:343749474543
DESCRIPTION:A Shanghai Academy of Spaceflight Technology (SAST) Long Marc
 h (Chang Zheng) CZ-6A rocket will launch the Yaogan 50-03 (遥感五十号
 03星) remote sensing satellite into a retrograde low Earth orbit. It is r
 eportedly tasked with land surveys\, crop yield estimation\, as well as di
 saster prevention and mitigation.
LOCATION:Launch Complex 9A - Taiyuan Satellite Launch Center https://goo.g
 l/maps/K35kt5KCe1sToeii9
END:VEVENT
BEGIN:VEVENT
SUMMARY:Long March CZ-4B • Yaogan 54 Group 1 & Yaogan 55 Group 1
DTSTART;VALUE=DATE-TIME:20261023T192500Z
DTEND;VALUE=DATE-TIME:20261023T192500Z
UID:106064547486
DESCRIPTION:A Shanghai Academy of Spaceflight Technology (SAST) Long Marc
 h (Chang Zheng) CZ-4B rocket launched two triplets of Yaogan 54 and 55 rem
 ote sensing satellites (designated Yaogan 54-01 to 54-03 and Yaogan 55-01 
 to 55-03\, 遥感五十四01-0)卫星\, 遥感五十五01-03卫星) into o
 rbit. All six remote sensing satellites were developed by the China Academ
 y of Space Technology.\n-\nDelayed from Oct. 14.\n\nPossible webcast: http
 s://www.youtube.com/live/flD-zMUCW6I
LOCATION:LC-43/94 (Pad 601 / South Launch Site 2) - Jiuquan Satellite Laun
 ch Center https://goo.gl/maps/CfKcRo56gcVCiLtL9
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • Starlink 12981–13007
DTSTART;VALUE=DATE-TIME:20261023T220000Z
DTEND;VALUE=DATE-TIME:20261023T220000Z
UID:202531235279
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 27 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 15-15 and the booster is designated as B1
 063.36 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mi
 ni Optimized satellites are built by SpaceX and have a reported launch mas
 s of 575kg. The mass-produced spacecraft carry a communications payload us
 ing the Ku and Ka frequency bands\, plus E-band for backhaul\, which will 
 allow Starlink to provide ~4x more capacity per satellite than earlier ite
 rations. They also employ optical inter-satellite links\, phased array bea
 m forming and digital processing technologies. On the v2 sats the Krypton 
 thrusters are replaced with new and more powerful Argon Hall thrusters. Th
 e Optimized chassis features upgrades\, such as a new backhaul antenna wit
 h a SpaceX-designed and built dual-band chip and improved avionics\, propu
 lsion and power systems. Starlink sats are able to track on-orbit debris a
 nd capable of autonomous collision avoidance. All satellites will be equip
 ped with anti-reflective coatings.\nThe updated Starlink network architect
 ure has 1584 satellites at 550km altitude and an inclination of 53 degrees
 \, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satel
 lites at 570km and an inclination of 70 degrees\, and 520 satellites at 56
 0km and an inclination of 97.6 degrees. The initial FCC application covere
 d 4408 Starlink satellites. Eventually SpaceX will launch and operate a fo
 llow-on network of 7518 additional Starlink satellites transmitting in V-b
 and frequencies. In the final deployment stage an additional 30000 Starlin
 k satellites might get orbited.\n-\nScrubbed on Oct. 20\, 21 and 22.\n\nWe
 bcast: https://x.com/i/broadcasts/1YGNrbnzdqLGw\nhttps://www.spacex.com/l
 aunches/sl-15-15\nhttps://www.youtube.com/live/d4zn2Tth8O0\nhttps://spacef
 lightnow.com/2026/10/20/live-coverage-spacex-to-launch-27-starlink-satelli
 tes-on-falcon-9-rocket-from-vandenberg-sfb-5/\nhttps://www.youtube.com/liv
 e/1WIYKNxTLzA\nhttps://www.youtube.com/live/flWsFi70wck\nhttps://www.youtu
 be.com/live/k-TFfeJD8T4
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:Long March CZ-8A • Guowang
DTSTART;VALUE=DATE-TIME:20261025T025700Z
DTEND;VALUE=DATE-TIME:20261025T025700Z
UID:330272398911
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.\n-\
 nDelayed from Oct. 22.
LOCATION:Pad 1 - Hainan Commercial Launch Site https://maps.app.goo.gl/2na
 KfJxVaF8UG7J59
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20261027T044500Z
DTEND;VALUE=DATE-TIME:20261027T044500Z
UID:253252979254
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 27 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 15-16 and the booster is designated as B1
 082.26 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mi
 ni Optimized satellites are built by SpaceX and have a reported launch mas
 s of 575kg. The mass-produced spacecraft carry a communications payload us
 ing the Ku and Ka frequency bands\, plus E-band for backhaul\, which will 
 allow Starlink to provide ~4x more capacity per satellite than earlier ite
 rations. They also employ optical inter-satellite links\, phased array bea
 m forming and digital processing technologies. On the v2 sats the Krypton 
 thrusters are replaced with new and more powerful Argon Hall thrusters. Th
 e Optimized chassis features upgrades\, such as a new backhaul antenna wit
 h a SpaceX-designed and built dual-band chip and improved avionics\, propu
 lsion and power systems. Starlink sats are able to track on-orbit debris a
 nd capable of autonomous collision avoidance. All satellites will be equip
 ped with anti-reflective coatings.\nThe updated Starlink network architect
 ure has 1584 satellites at 550km altitude and an inclination of 53 degrees
 \, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satel
 lites at 570km and an inclination of 70 degrees\, and 520 satellites at 56
 0km and an inclination of 97.6 degrees. The initial FCC application covere
 d 4408 Starlink satellites. Eventually SpaceX will launch and operate a fo
 llow-on network of 7518 additional Starlink satellites transmitting in V-b
 and frequencies. In the final deployment stage an additional 30000 Starlin
 k satellites might get orbited.\n-\nDelayed from Oct. 24 and 26.\n\nWebcas
 t: \nhttps://www.spacex.com/launches/sl-15-16\n\nhttps://spaceflightnow.c
 om/
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
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 40 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:Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20261030T040200Z
DTEND;VALUE=DATE-TIME:20261030T040200Z
UID:516316293905
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 27 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 15-18 and the booster is designated as B1
 093.18 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mi
 ni Optimized satellites are built by SpaceX and have a reported launch mas
 s of 575kg. The mass-produced spacecraft carry a communications payload us
 ing the Ku and Ka frequency bands\, plus E-band for backhaul\, which will 
 allow Starlink to provide ~4x more capacity per satellite than earlier ite
 rations. They also employ optical inter-satellite links\, phased array bea
 m forming and digital processing technologies. On the v2 sats the Krypton 
 thrusters are replaced with new and more powerful Argon Hall thrusters. Th
 e Optimized chassis features upgrades\, such as a new backhaul antenna wit
 h a SpaceX-designed and built dual-band chip and improved avionics\, propu
 lsion and power systems. Starlink sats are able to track on-orbit debris a
 nd capable of autonomous collision avoidance. All satellites will be equip
 ped with anti-reflective coatings.\nThe updated Starlink network architect
 ure has 1584 satellites at 550km altitude and an inclination of 53 degrees
 \, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satel
 lites at 570km and an inclination of 70 degrees\, and 520 satellites at 56
 0km and an inclination of 97.6 degrees. The initial FCC application covere
 d 4408 Starlink satellites. Eventually SpaceX will launch and operate a fo
 llow-on network of 7518 additional Starlink satellites transmitting in V-b
 and frequencies. In the final deployment stage an additional 30000 Starlin
 k satellites might get orbited.\n-\nDelayed from Oct. 28 and 29.\n\nWebcas
 t: \nhttps://www.spacex.com/launches/sl-15-18\n\nhttps://spaceflightnow.c
 om/
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:GSLV Mk.II • NavIC 12
DTSTART;VALUE=DATE-TIME:20261030T170000Z
DTEND;VALUE=DATE-TIME:20261030T170000Z
UID:234632347107
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) Alpha B2 • ConnectedCosmos 3–8
DTSTART;VALUE=DATE:20261030
DTEND;VALUE=DATE:20261031
UID:268415925763
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) Tianlong TL-3 • Test Flight
DTSTART;VALUE=DATE:20261030
DTEND;VALUE=DATE:20261031
UID:157481461360
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) Kinetica 1 • TBD
DTSTART;VALUE=DATE:20261030
DTEND;VALUE=DATE:20261031
UID:250961340627
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) Kinetica 2 • Qianfan
DTSTART;VALUE=DATE:20261030
DTEND;VALUE=DATE:20261031
UID:692935746435
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:(TBD) Gravity YL-2 • Test Flight
DTSTART;VALUE=DATE:20261031
DTEND;VALUE=DATE:20261101
UID:267128147215
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: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) Falcon 9 B5 • Globalstar
DTSTART;VALUE=DATE:20261101
DTEND;VALUE=DATE:20261102
UID:145423578791
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch 9 new generation 
 Globalstar communications satellites (designated as HIBLEO-4) into low Ear
 th orbit (LEO). Globalstar M11?–M11? will be the 106th to 114th satellit
 es launched for Globalstar's constellation. Globalstar reserves 85% of its
  network capacity for Apple’s Emergency SOS via Satellite service. The s
 eventeen 500kg satellites under this contract\, built by MDA with Lightnin
 g buses supplied by Rocket Lab\, are intended to sustain and grow that cap
 acity through the middle of the next decade. Each satellite is also expect
 ed to support Globalstar’s broader Band 53 terrestrial-spectrum services
 . The flight is known as Globalstar 2-R Launch 2 and the Falcon 9 booster 
 is designated as B10XX.X for this mission and will perform a RTLS landing 
 at LZ-40. The second stage will fly with a shortened nozzle and a reused f
 airing.\n-\nDelayed from late October.\n\nWebcast: \nhttps://www.spacex.co
 m/launches/globalstar2-rlaunch2\n\nhttps://spaceflightnow.com/
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate
 n
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) 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) 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) SSLV • AayulSAT 1A & CubeSat
DTSTART;VALUE=DATE:20261101
DTEND;VALUE=DATE:20261102
UID:338893489697
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\, 2025 and October.
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) New Glenn 7×2 • BR-1
DTSTART;VALUE=DATE:20261101
DTEND;VALUE=DATE:20261102
UID:326165727950
DESCRIPTION:A Blue Origin New Glenn rocket will launch on its third flight
 \, carrying the Blue Ring 1 (BR-1) spacecraft into orbit. Powered by a sin
 gle hydroLOX-fueled BE-7 engine\, the lander will aim to touch down within
  10m of its intended target at Shackleton crater. New Glenn version 7×2 i
 s equipped with seven BE-4 LNG/LOX engines on the reusable GS1 first stage
  and two BE-3U hydroLOX engines on the GS2 second stage.\n-\nDelayed from 
 H1 2026.
LOCATION:Space Launch Complex 36\, air force station\, Cape Canaveral\, FL
  32920\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Long March CZ-12A • Test Flight
DTSTART;VALUE=DATE:20261102
DTEND;VALUE=DATE:20261103
UID:186218024350
DESCRIPTION:A Shanghai Academy of Spaceflight Technology (SAST) Long Marc
 h (Chang Zheng) CZ-12A rocket will launch on its first flight. The first s
 tage was previously used as a hopper for test flights. The two stage CZ-12
 A rocket is powered by 7 Longyun methaLOX engines on the first stage while
  its second stage is propelled by one YF-209V methaLOX engine. The first s
 tage is built to be reusable and features recovery hardware like gridfins 
 and landing legs.\n-\nDelayed from September.
LOCATION:China Rocket Research & Test Launch Station - Jiuquan Satellite L
 aunch Center
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • QPS-SAR 20
DTSTART;VALUE=DATE:20261103
DTEND;VALUE=DATE:20261104
UID:297144262775
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch the QPS-SAR 20 satellite (Wadstsumi-II) for iQPS of Japan. Roc
 ket Lab's mission will be named "The Sea God Surveys" and fly with an exte
 nded fairing.\n-\nQ-shu Pioneers of Space – Synthetic Aperture Radar (QP
 S-SAR) are operational satellites in a series of small high-resolution rad
 ar Earth observation sats by the QPS Institute (iQPS). The 100kg satellite
 s feature a 3.6m diameter antenna of only 10kg. It can distinguish objects
  1 meter long and identify cars on the road. Compared to the prototypes (Q
 PS-SAR 1\, 2)\, these satellites have increased power due to two deployabl
 e solar arrays and increased battery capacity. They also feature thrusters
  for station keeping. The full constellation will have 36 satellites.\n\nW
 ebcast: \nhttps://rocketlabcorp.com/live-stream/
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20261105T051400Z
DTEND;VALUE=DATE-TIME:20261105T051400Z
UID:164660835401
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 27 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 15-21 and the booster is designated as B1
 103.7 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Min
 i Optimized satellites are built by SpaceX and have a reported launch mass
  of 575kg. The mass-produced spacecraft carry a communications payload usi
 ng the Ku and Ka frequency bands\, plus E-band for backhaul\, which will a
 llow Starlink to provide ~4x more capacity per satellite than earlier iter
 ations. They also employ optical inter-satellite links\, phased array beam
  forming and digital processing technologies. On the v2 sats the Krypton t
 hrusters are replaced with new and more powerful Argon Hall thrusters. The
  Optimized chassis features upgrades\, such as a new backhaul antenna with
  a SpaceX-designed and built dual-band chip and improved avionics\, propul
 sion and power systems. Starlink sats are able to track on-orbit debris an
 d capable of autonomous collision avoidance. All satellites will be equipp
 ed with anti-reflective coatings.\nThe updated Starlink network architectu
 re has 1584 satellites at 550km altitude and an inclination of 53 degrees\
 , 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satell
 ites at 570km and an inclination of 70 degrees\, and 520 satellites at 560
 km and an inclination of 97.6 degrees. The initial FCC application covered
  4408 Starlink satellites. Eventually SpaceX will launch and operate a fol
 low-on network of 7518 additional Starlink satellites transmitting in V-ba
 nd frequencies. In the final deployment stage an additional 30000 Starlink
  satellites might get orbited.\n-\nDelayed from Nov. 1.\n\nWebcast: \nhtt
 ps://www.spacex.com/launches/sl-15-21\n\nhttps://spaceflightnow.com/
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • NROL-195
DTSTART;VALUE=DATE-TIME:20261105T223400Z
DTEND;VALUE=DATE-TIME:20261105T223400Z
UID:317018484301
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the classified NR
 OL-195 mission for the National Reconnaissance Office. It is for the first
  phase of NRO's imaging satellite constellation built by SpaceX and Northr
 op Grumman and is understood to be the 15th of multiple batches to launch.
  The NRO's Proliferated Architecture is a constellation of intelligence sa
 tellites\, including imaging and relay satellites. The 9? satellites on th
 is launch are built upon SpaceX' Starshield bus\, with Northrop Grumman pr
 oviding sensors for some of them. The booster is designated B1XXX.X for th
 is mission and will perform a RTLS landing at LZ-4.\n\nWebcast: \nhttps:/
 /www.spacex.com/launches/nrol195\n\nhttps://spaceflightnow.com/
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
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
BEGIN:VEVENT
SUMMARY:(NET) Electron • QPS-SAR 19
DTSTART;VALUE=DATE:20261110
DTEND;VALUE=DATE:20261111
UID:206235486710
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch the QPS-SAR 19 satellite (named ?) for iQPS of Japan. Rocket L
 ab's mission will be named "The Mountain God Rises" and fly with an extend
 ed fairing.\n-\nQ-shu Pioneers of Space – Synthetic Aperture Radar (QPS-
 SAR) are operational satellites in a series of small high-resolution 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. Compared to the prototypes (QPS
 -SAR 1\, 2)\, these satellites have increased power due to two deployable 
 solar arrays and increased battery capacity. They also feature thrusters f
 or station keeping. The full constellation will have 36 satellites.\n\nWeb
 cast: \nhttps://rocketlabcorp.com/live-stream/
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • TBD
DTSTART;VALUE=DATE:20261115
DTEND;VALUE=DATE:20261116
UID:234944319340
DESCRIPTION:A Rocket Lab Electron rocket topped with a modified upper stag
 e will launch on a HASTE (Hypersonic Accelerator Suborbital Test Electron)
  suborbital mission\, designated "?"\, for an unknown customer (probably 
 Anduril).
LOCATION:LC2\, 41 N Seawall Rd\, Wallops Island\, VA 23337\, Vereinigte St
 aaten
END:VEVENT
END:VCALENDAR