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BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • Transporter-15
DTSTART;VALUE=DATE-TIME:20251110T181800Z
DTEND;VALUE=DATE-TIME:20251110T181800Z
UID:288740557610
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch several smallsats
  on the Transporter-15 rideshare mission to Sun-synchronous orbit. Onboard
  is LEO Express 3\, which is a Mira OTV (Orbital Tug Vehicle) by Impulse 
 Space. Part of the payloads is also ESA's second Earth observation Scout m
 ission\, HydroGNSS\, which will provide measurements of key hydrological c
 limate variables\, including soil moisture\, freeze–thaw state over perm
 afrost\, inundation and wetlands\, and above-ground biomass\, using a tech
 nique called Global Navigation Satellite System (GNSS) reflectometry. The 
 satellite measures the signal reflected off the land\, ice and ocean from 
 existing GNSS missions such as Galileo and GPS. Although these signals are
  faint\, they can be collected by a low power receiver that can be accommo
 dated on a small satellite in low Earth orbit making it compatible with a 
 Scout mission. The mission will complement missions such as ESA's SMOS and
  Biomass\, Copernicus Sentinel 1 and NASA's SMAP. The Mauve space telescop
 e and 8 IRIDE satellites for Italy's ASI will also be on this flight. The
  booster is designated B10XX.X for this mission and will perform a RTLS (r
 eturn to launch site) at LZ-4.\n-\nDelayed from October.\n\nWebcast: \nhtt
 ps://www.spacex.com/launches\nhttps://spaceflightnow.com
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20251110T221200Z
DTEND;VALUE=DATE-TIME:20251110T221200Z
UID:118724286349
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 29 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 6-87 and the booster is designated as B10
 96.3 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mini
  Optimized satellites are built by SpaceX and have a reported launch mass 
 of 575kg. The mass-produced spacecraft carry a communications payload usin
 g the Ku and Ka frequency bands\, plus E-band for backhaul\, which will al
 low Starlink to provide ~4x more capacity per satellite than earlier itera
 tions. They also employ optical inter-satellite links\, phased array beam 
 forming and digital processing technologies. On the v2 sats the Krypton th
 rusters are replaced with new and more powerful Argon Hall thrusters. The 
 Optimized chassis features upgrades\, such as a new backhaul antenna with 
 a SpaceX-designed and built dual-band chip and improved avionics\, propuls
 ion and power systems. Starlink sats are able to track on-orbit debris and
  capable of autonomous collision avoidance. All satellites will be equippe
 d with anti-reflective coatings.\nThe updated Starlink network architectur
 e has 1584 satellites at 550km altitude and an inclination of 53 degrees\,
  1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satelli
 tes at 570km and an inclination of 70 degrees\, and 520 satellites at 560k
 m and an inclination of 97.6 degrees. The initial FCC application covered 
 4408 Starlink satellites. Eventually SpaceX will launch and operate a foll
 ow-on network of 7518 additional Starlink satellites transmitting in V-ban
 d frequencies. In the final deployment stage an additional 30000 Starlink 
 satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/launch
 es/mission/?missionId=sl-6-87\n\nhttps://spaceflightnow.com/
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20251113T223500Z
DTEND;VALUE=DATE-TIME:20251113T223500Z
UID:134878716670
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 29 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 6-89 and the booster is designated as B10
 92.8 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Mini
  Optimized satellites are built by SpaceX and have a reported launch mass 
 of 575kg. The mass-produced spacecraft carry a communications payload usin
 g the Ku and Ka frequency bands\, plus E-band for backhaul\, which will al
 low Starlink to provide ~4x more capacity per satellite than earlier itera
 tions. They also employ optical inter-satellite links\, phased array beam 
 forming and digital processing technologies. On the v2 sats the Krypton th
 rusters are replaced with new and more powerful Argon Hall thrusters. The 
 Optimized chassis features upgrades\, such as a new backhaul antenna with 
 a SpaceX-designed and built dual-band chip and improved avionics\, propuls
 ion and power systems. Starlink sats are able to track on-orbit debris and
  capable of autonomous collision avoidance. All satellites will be equippe
 d with anti-reflective coatings.\nThe updated Starlink network architectur
 e has 1584 satellites at 550km altitude and an inclination of 53 degrees\,
  1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satelli
 tes at 570km and an inclination of 70 degrees\, and 520 satellites at 560k
 m and an inclination of 97.6 degrees. The initial FCC application covered 
 4408 Starlink satellites. Eventually SpaceX will launch and operate a foll
 ow-on network of 7518 additional Starlink satellites transmitting in V-ban
 d frequencies. In the final deployment stage an additional 30000 Starlink 
 satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/launch
 es/mission/?missionId=sl-6-89\n\nhttps://spaceflightnow.com/
LOCATION:SpaceX LC-39A\, Florida\, Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:Atlas V 551 • ViaSat 3-F2
DTSTART;VALUE=DATE-TIME:20251114T030000Z
DTEND;VALUE=DATE-TIME:20251114T034400Z
UID:811148798995
DESCRIPTION:A United Launch Alliance Atlas V rocket\, designated AV-100\, 
 will launch the ViaSat 3-F2 (VS-3 F2) satellite into GTO. ViaSat 3-F2 is t
 he second of at least three new-generation Boeing-built geostationary sate
 llites for Viasat. Due to technical difficulties with F1 that significantl
 y lowered its capacity\, once F2 is launched it will cover the Americas\, 
 and F1 will be moved to the EMEA region. Atlas will fly in the 551 vehicle
  configuration with a five-meter fairing\, five GEM-63 solid rocket booste
 rs and a single-engine Centaur upper stage.\n\nMission profile video: http
 s://youtu.be/ldX_Z7KfNq4\nhttps://x.com/ulalaunch/status/19838738469158300
 02\n-\nThe 6.4 tonne Viasat 3-F2 (VS-3 F2) satellite is as big as a school
  bus\, and its solar panels will unfurl in orbit to generate more than 30 
 kilowatts of power in orbit. The spacecraft has one of the largest antenna
  reflectors ever sent into space\, and will rely on all-electric propulsio
 n for fine orbital maneuvers and station-keeping.\nThe ViaSat 3 constellat
 ion of high capacity broadband satellites for ViaSat Inc consists of three
  satellites for global coverage. Boeing was selected to provide the all-el
 ectric propulsion BSS-702MP+ (originally BSS-702HP were to be used) busses
 \, while the communications payloads were built by ViaSat. Each ViaSat 3 c
 lass satellite is expected to offer over 1 Terabit per second (Tbps) of to
 tal network capacity to deliver a global broadband network with enough ban
 dwidth to deliver affordable\, high-speed\, high-quality internet and vide
 o streaming services.\n-\nDelayed from March\, June\, July\, September 202
 2\, March 31\, September 2023\, Q1\, June\, December 2024\, March and Nov.
  4. Scrubbed on Nov. 6 and 7.\n\nWebcast: https://www.youtube.com/live/DWg
 oYkFr-HE\nhttps://www.ulalaunch.com/missions/next-launch/atlas-v-viasat-3-
 f2\nhttps://youtu.be/QJJ5myya1t0\nhttps://spaceflightnow.com/2025/11/05/li
 ve-coverage-ula-to-launch-viasat-3-communications-satellite-on-atlas-5-roc
 ket-from-cape-canaveral/\nhttps://www.youtube.com/live/3dp3jYTkkGQ\nhttps:
 //www.youtube.com/live/tEyv3wqF4cM\nhttps://www.youtube.com/live/L5DyzO4aT
 ec
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:20251114T211200Z
DTEND;VALUE=DATE-TIME:20251114T211200Z
UID:128193347972
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 28 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 6-85 and the booster is designated as B10
 78.24 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Min
 i Optimized satellites are built by SpaceX and have a reported launch mass
  of 575kg. The mass-produced spacecraft carry a communications payload usi
 ng the Ku and Ka frequency bands\, plus E-band for backhaul\, which will a
 llow Starlink to provide ~4x more capacity per satellite than earlier iter
 ations. They also employ optical inter-satellite links\, phased array beam
  forming and digital processing technologies. On the v2 sats the Krypton t
 hrusters are replaced with new and more powerful Argon Hall thrusters. The
  Optimized chassis features upgrades\, such as a new backhaul antenna with
  a SpaceX-designed and built dual-band chip and improved avionics\, propul
 sion and power systems. Starlink sats are able to track on-orbit debris an
 d capable of autonomous collision avoidance. All satellites will be equipp
 ed with anti-reflective coatings.\nThe updated Starlink network architectu
 re has 1584 satellites at 550km altitude and an inclination of 53 degrees\
 , 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satell
 ites at 570km and an inclination of 70 degrees\, and 520 satellites at 560
 km and an inclination of 97.6 degrees. The initial FCC application covered
  4408 Starlink satellites. Eventually SpaceX will launch and operate a fol
 low-on network of 7518 additional Starlink satellites transmitting in V-ba
 nd frequencies. In the final deployment stage an additional 30000 Starlink
  satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/launc
 hes/mission/?missionId=sl-6-85\n\nhttps://spaceflightnow.com/
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Ceres 2 • Zidingxiang 3
DTSTART;VALUE=DATE:20251115
DTEND;VALUE=DATE:20251116
UID:316269160880
DESCRIPTION:A Galactic Energy Ceres 2 (Gushenxing 2\, GX-2) rocket will la
 unch on its first flight\, with six commercial satellites and two insepara
 ble payloads\, totaling over one ton. Part of the manifest will be Zidingx
 iang 3 (紫丁香三号\, Lilac 3\, also known as Space Chain 1)\, which i
 s an ultra-flat disk satellite. Zidingxiang 3 will carry out a number of n
 ew technology tests including ultra-flat thermal and mechanical integrated
  configuration\, new attitude control\, and atmospheric drag orbit control
 . The mission is named "Yueyunjin". The three stage solid-fueled Ceres 2 r
 ocket is topped with a liquid-fueled upper stage.\n-\nDelayed from June\, 
 August and September.
LOCATION:LC-43/95A - Jiuquan Satellite Launch Center https://goo.gl/maps/p
 bNBUb1duneU9V2n6
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Zhuque ZQ-3 • Test Flight
DTSTART;VALUE=DATE:20251115
DTEND;VALUE=DATE:20251116
UID:882983717883
DESCRIPTION:A Landspace Zhuque ZQ-3 rocket will launch on its first test f
 light. The debut ZQ-3 vehicle is understood to be shorter and have a reduc
 ed capacity. Its first stage will return for a landing attempt. The Zhuque
  3 rocket is equipped with nine TQ-12B methaLOX engines on the reusable fi
 rst stage and the second stage features a TQ-15B engine optimised for oper
 ation in vacuum.\n-\nMoved forward from late 2025. Delayed from June and O
 ctober.
LOCATION:LC-43/96B - Jiuquan Satellite Launch Center https://maps.app.goo.
 gl/wCtwtpgk3NDNoAfd6
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • OTC-P2
DTSTART;VALUE=DATE:20251115
DTEND;VALUE=DATE:20251116
UID:281196099914
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch eight wildfire monitoring infrared satellites for OroraTech. Th
 ey are built to the 6U CubeSat form factor and based on the FOREST 3 proto
 type satellite. The mission will deliver the Constellation Phase 2 satelli
 tes to a 550km orbit to expand its constellation providing data from space
  to help tackle wildfire challenges globally. OroraTech wants to deploy a 
 constellation of up to 100 satellites by 2028. Rocket Lab's mission will b
 e named "?".\n\nWebcast: \nhttps://www.rocketlabusa.com/live-stream\nhttp
 s://spaceflightnow.com/
LOCATION:LC-1B\, PVQ8+R3\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • Arirang 7A
DTSTART;VALUE=DATE:20251115
DTEND;VALUE=DATE:20251116
UID:329129016025
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch with the Arirang
  7A (아리랑 7A\, KOMPSAT 7A) satellite for KARI. Arirang 7A is a follo
 w-up model of (Korean Multi-purpose Satellite) KOMPSAT 3A. Arirang 7A wi
 ll be equipped with the high resolution spaceborne camera named AEISS-HR (
 Advanced Earth Imaging Sensor System with High Resolution)\, which possess
 es 30cm resolution in panchromatic mode\, 1.2m in color mode\, and 4m in i
 nfra-red mode. The booster is designated B10XX.X for this mission.\n-\nDe
 layed from September.\n\nWebcast: \nhttps://www.spacex.com/launches\nhttps
 ://spaceflightnow.com
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, Vereinigte Staate
 n
END:VEVENT
BEGIN:VEVENT
SUMMARY:Electron • Van
DTSTART;VALUE=DATE-TIME:20251116T124500Z
DTEND;VALUE=DATE-TIME:20251116T124500Z
UID:259441567363
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 Van.
LOCATION:LC2\, 41 N Seawall Rd\, Wallops Island\, VA 23337\, Vereinigte St
 aaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • Sentinel 6B
DTSTART;VALUE=DATE:20251116
DTEND;VALUE=DATE:20251117
UID:203893819873
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the Sentinel 6B (
 Jason-CS B) radar altimeter mission in a continuation of the existing part
 nership for Jason 3 between Europe (ESA and Eumetsat) and the US (NOAA and
  NASA). It will be part of the Copernicus program. The Jason-CS (Jason Con
 tinuity of Service) mission will consist of two Sentinel 6 satellites. ESA
  was responsible for the development of the Sentinel 6A satellite\, the pr
 ototype processors\, delivery of the LEOP services\, and the procurement o
 f the recurrent satellite on behalf of EUMETSAT and the European Commissio
 n (EC). EUMETSAT is leading the system definition and is responsible for t
 he Jason-CS ground segment development\; operations preparation and operat
 ions of both satellites\, and co-funded the Sentinel 6B satellite\, togeth
 er with the EC. The European Commission also funds the operations of both
  Sentinel 6 satellites\, including the LEOP service for the second Sentine
 l 6B satellite. NOAA provides the launch services for both Sentinel 6 sate
 llites\, US payload instruments and ground segment support and will contri
 bute to the operations. The Falcon 9 booster is designated as B10XX for th
 is flight.\n\nMission profile video: https://twitter.com/Falcon_1e/status/
 1315009212716445696\n-\nThe Sentinel 6B spacecraft was built by Airbus Def
 ence and Space at their Friedrichshafen facility in Germany. It's 5.15m in
  length\, 2.35m in height\, and 2.58m in width. The satellite weighs appro
 ximately 1192kg when fully fueled for launch. The Sentinel 6 spacecrafts a
 re based on a platform derived from CryoSat 2\, but adjusted to the specif
 ic requirements of the Jason-CS mission and specific orbit. The orbit will
  remain the same as the earlier Jason orbit - non-sun-synchronous\, 1336 k
 m\, 66° inclination. The satellites are equipped with the following instr
 uments: A radar altimeter developed by ESA\, an AMR-C microwave radiometer
  provided by NOAA\, a GNSS Precise Orbit Determination (POD) receiver deve
 loped by ESA\, the same DORIS Receiver as on Jason 3 and Sentinel 3\, the 
 same Laser Reflector Array as on Jason 3 and a radio-occultation instrumen
 t based on a Tri-G receiver\, provided by NOAA. Sentinel 6 satellites have
  a planned orbital lifetime of 5.5 years.
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20251118T110000Z
DTEND;VALUE=DATE-TIME:20251118T110000Z
UID:167563838607
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 28 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 6-94 and the booster is designated as B10
 85.12 for this mission\, flying with a reused fairing.\n-\nStarlink v2 Min
 i Optimized satellites are built by SpaceX and have a reported launch mass
  of 575kg. The mass-produced spacecraft carry a communications payload usi
 ng the Ku and Ka frequency bands\, plus E-band for backhaul\, which will a
 llow Starlink to provide ~4x more capacity per satellite than earlier iter
 ations. They also employ optical inter-satellite links\, phased array beam
  forming and digital processing technologies. On the v2 sats the Krypton t
 hrusters are replaced with new and more powerful Argon Hall thrusters. The
  Optimized chassis features upgrades\, such as a new backhaul antenna with
  a SpaceX-designed and built dual-band chip and improved avionics\, propul
 sion and power systems. Starlink sats are able to track on-orbit debris an
 d capable of autonomous collision avoidance. All satellites will be equipp
 ed with anti-reflective coatings.\nThe updated Starlink network architectu
 re has 1584 satellites at 550km altitude and an inclination of 53 degrees\
 , 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 satell
 ites at 570km and an inclination of 70 degrees\, and 520 satellites at 560
 km and an inclination of 97.6 degrees. The initial FCC application covered
  4408 Starlink satellites. Eventually SpaceX will launch and operate a fol
 low-on network of 7518 additional Starlink satellites transmitting in V-ba
 nd frequencies. In the final deployment stage an additional 30000 Starlink
  satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/launc
 hes/mission/?missionId=sl-6-94\n\nhttps://spaceflightnow.com/
LOCATION:Space Launch Complex 40\, Cape Canaveral\, FL\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:Long March CZ-8A • Guowang 131–139
DTSTART;VALUE=DATE-TIME:20251119T130000Z
DTEND;VALUE=DATE-TIME:20251119T130000Z
UID:273146559762
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 14 (卫星互联网低轨14组) an
 d the satellites are designated as Hulianwang Digui 14A/B/C/D/E/F/G/H/I.\n
 -\nThe Guowang satellite program can carry a variety of payloads\, includi
 ng broadband communication payloads\, laser communication payloads\, synth
 etic aperture radar payloads\, optical remote sensing payloads\, and other
 s\, to meet the needs of different users and scenarios. It offers comprehe
 nsive technical support across numerous fields such as maritime and aviati
 on operations\, information security\, navigation and positioning\, and me
 teorological research\, while also enabling expansion into the global sate
 llite internet access market. The eventual constellation is expected to gr
 ow to 12992 satellites. This will be made up of 6080 in the low orbit GW-A
 59 sub-constellation at altitudes below 500km\, offering initial broadband
  coverage. The rest will orbit in the higher GW-A2 sub-constellation at 11
 45 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:Falcon 9 B5 • Starlink
DTSTART;VALUE=DATE-TIME:20251119T220000Z
DTEND;VALUE=DATE-TIME:20251119T220000Z
UID:336410817459
DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 28 Sta
 rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in
 ternally known as Starlink Group 11-30 and the booster is designated as B1
 071.30 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\nWebcast: \nhttps://www.spacex.com/laun
 ches/sl-11-30\n\nhttps://spaceflightnow.com/
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) New Shepard • Mission NS-37
DTSTART;VALUE=DATE:20251120
DTEND;VALUE=DATE:20251121
UID:338123020146
DESCRIPTION:Blue Origin will launch its New Shepard suborbital rocket (boo
 ster designation Tail 5 or NS5) on a crewed mission named NS-37. Hans Kön
 igsmann\, Michaela Benthaus\, and ? will be part of the crew. The capsule
  used for this flight is CC 2.0-3 RSS Kármán line.
LOCATION:Blue Origin Launch Site One\, Culberson County\, Texas\, Vereinig
 te Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • QPS-SAR 13
DTSTART;VALUE=DATE:20251120
DTEND;VALUE=DATE:20251121
UID:259169106447
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch the QPS-SAR 13 satellite (named ?) for iQPS of Japan. Rocket L
 ab's mission will be named "?" and fly with an extended fairing.\n-\nQ-shu
  Pioneers of Space – Synthetic Aperture Radar (QPS-SAR) are operational 
 satellites in a series of small high-resolution SAR (synthetic aperture ra
 dar) Earth observation sats by the QPS Institute (iQPS). The 100kg satelli
 tes feature a 3.6m diameter antenna of only 10kg. It can distinguish objec
 ts 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 deploya
 ble solar arrays and increased battery capacity. They also feature thruste
 rs for station keeping. The planned constellation will have 36 satellites.
 \n\nWebcast: \nhttps://rocketlabcorp.com/live-stream/
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • PWSA
DTSTART;VALUE=DATE:20251120
DTEND;VALUE=DATE:20251121
UID:798945636743
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 ?) on this flight are for the Transport Layer and were built
  by ?. The mission is designated as SDA-T1TL-A and the Falcon 9 booster is
  B10XX.X for this flight. The 2nd stage is equipped with a Mission Extensi
 on Kit. Comprising a gray band on the RP-1 tank\, extra helium bottles & b
 atteries\, this kit extends the life of the stage in-orbit\, allowing it t
 o deploy the payload directly into its operational orbit.\n-\nOnce fully o
 perational\, the SDA Transport Layer will consist of a proliferated hetero
 geneous constellation of data relay space vehicles (SVs) that provide pers
 istent global coverage through a mesh network comprised of communication s
 atellites that connect to one another and to other space vehicles and grou
 nd stations via optical intersatellite links (OISLs). By nature of the mes
 h network spanning the globe\, the Transport satellites will also be able 
 to transmit precise position\, navigation and timing (PNT) data to enhance
  GPS. A-class satellites have at least four optical cross-links\, that is 
 so they can talk to satellites that are in plane with one another as they'
 re traveling and they also can talk to satellites that are cross-plane or 
 in completely different orbits. So they can maintain those four lines of c
 ommunication simultaneously. The B-class satellites will connect directly 
 to the warfighters via the Link-16 military communications system. They ha
 ve two optical cross-links each\, so that allows them to maintain constant
  communication with the other transport satellites in plane. The two other
  nodes will be Link-16 transmitters. Link-16 is an existing tactical commu
 nication system used across the services primarily for air and ground syst
 ems to share low latency data.The first phase of SDA’s Proliferated Warf
 ighter Space Architecture consists of 28 satellites (Tranche 0 including 2
 0 communications payloads made by Lockheed Martin and York Space\, and eig
 ht missile-tracking infrared sensor satellites made by SpaceX and Leidos) 
 as a proof of concept for the missile tracking and data relay network\, fo
 llowed by more than 150 additional satellites to provide an initial operat
 ional capability. In total\, Tranche 1 will consist of 154 operational sat
 ellites: 126 in the transport layer developed by York\, Northrop Grumman\,
  and Lockheed Martin\, and 28 focused on missile warning and tracking deve
 loped by Northrop Grumman and L3Harris. Combining conventional tactical ra
 dio links\, laser inter-satellite communications\, and wide-view infrared 
 sensors\, hundreds more SDA spacecraft could launch later as the Pentagon 
 ramps up efforts and integrates new capabilities.\n-\nDelayed from Septemb
 er\, December\, Q2 and October.\n\nWebcast:\nhttps://www.spacex.com/launch
 es\nhttps://spaceflightnow.com
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC2S • GPS III-8
DTSTART;VALUE=DATE:20251120
DTEND;VALUE=DATE:20251121
UID:534244499519
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated ?\, will l
 aunch the U.S. Air Force’s ninth third-generation navigation satellite f
 or the Global Positioning System\, designated GPS III Space Vehicle 09 (GP
 S III SV09\, named Ellison Onizuka) into Medium Earth Orbit. Vulcan will f
 ly in the VC2S vehicle configuration with a double-engine Centaur upper st
 age\, two solid rocket boosters and a standard fairing.
LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\
 , FL 32780\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Long March CZ-3B/E • TBD
DTSTART;VALUE=DATE-TIME:20251121T110000Z
DTEND;VALUE=DATE-TIME:20251121T110000Z
UID:323009048845
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. The launcher will fly as CZ-3B/G? variant.
LOCATION:Xichang Satellite Launch Center
END:VEVENT
BEGIN:VEVENT
SUMMARY:Hanbit-Nano LiMER • Jussara-K & GOLDS-UFSC
DTSTART;VALUE=DATE-TIME:20251122T180000Z
DTEND;VALUE=DATE-TIME:20251122T180000Z
UID:318486330773
DESCRIPTION:An Innospace Hanbit-Nano (한빛-나노) rocket will launch on
  its first orbital test flight\, after a Hanbit-TLV first stage performed 
 a successful suborbital test flight with a dummy second stage in 2023. It 
 will carry the Jussara-K 1U and GOLDS-UFSC CubeSats plus four other smalls
 ats as payload. Under contracts signed with five customers from Brazil\, I
 ndia\, and South Korea\, the launcher will deliver a total of eight regist
 ered payloads (small satellites and non-separating experimental payloads) 
 along with one symbolic branding item as a non-registered payload. The fiv
 e small satellites are for practical purposes such as climate and environm
 ental data collection\, technology development\, and education\, as well a
 s three non-separating experimental payloads for technology verification a
 nd data acquisition in space. The mission will be named "SPACEWARD". The K
 orean Hanbit-Nano launcher is equipped with an electric 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.\n\nMission profile video: https://youtu.be/fB5
 W7WjkVrM\n-\nDelayed from March\, July and September.\n\nWebcast: https://
 youtube.com/@innospace
LOCATION:Alcântara Rocket Launch Pad A1\, Alcântara - Maranhão\, 65250-
 000\, Brasilien
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vega C • Arirang 7
DTSTART;VALUE=DATE:20251125
DTEND;VALUE=DATE:20251126
UID:319998170965
DESCRIPTION:An Arianespace Vega C rocket\, designated VV28\, will launch w
 ith the Arirang 7 (아리랑 7\, KOMPSAT 7) satellite for KARI. Arirang 
 7 is a follow-up model of (Korean Multi-purpose Satellite) KOMPSAT 3A. Ari
 rang 7 will be equipped with the high resolution spaceborne camera named A
 EISS-HR (Advanced Earth Imaging Sensor System with High Resolution)\, whic
 h possesses 30cm resolution in panchromatic mode\, 1.2m in color mode\, an
 d 4m in infra-red mode.\n-\nDelayed from September\, late 2023 and Septemb
 er.
LOCATION:ELV\, 66PG+C22\, Carbet Toukan 97310\, Französisch-Guyana
END:VEVENT
BEGIN:VEVENT
SUMMARY:Nuri • CAS500 3 & CubeSats
DTSTART;VALUE=DATE-TIME:20251126T155400Z
DTEND;VALUE=DATE-TIME:20251126T161400Z
UID:264069877730
DESCRIPTION:A Korean Nuri (KSLV-II) rocket will launch the CAS500 3 satell
 ite into orbit for KARI. Secondary payloads are 12 CubeSats including BEE 
 1000\, ETRISat\, Sejong 4\, COSMIC\, JACK 003 and JACK 004.\n-\nDelayed fr
 om Apr. 1 2024.
LOCATION:Second Launch Pad - Naro Space Center\, 182-3 Yenae-ri\, Bongnae-
 myeon\, Goheung-gun\, Jeollanam-do\, Südkorea
END:VEVENT
BEGIN:VEVENT
SUMMARY:Soyuz 2.1a • Soyuz MS-28 / ISS 74S
DTSTART;VALUE=DATE-TIME:20251127T072600Z
DTEND;VALUE=DATE-TIME:20251127T072600Z
UID:259211011740
DESCRIPTION:A Roscosmos Soyuz 2.1a rocket will launch the crewed Soyuz spa
 cecraft to the International Space Station with Sergey Kud-Sverchkov\, Ser
 gey Mikaev and NASA astronaut Christopher Williams as members of the next 
 Expedition crew. The capsule will remain at the station for about six mont
 hs\, providing an escape pod for the residents.\n-\nDelayed from mid-Septe
 mber and Oct. 25.
LOCATION:Pad 31/6 - Baikonur Cosmodrome\, Kasachstan
END:VEVENT
BEGIN:VEVENT
SUMMARY:Long March CZ-7A • TBD
DTSTART;VALUE=DATE-TIME:20251130T110000Z
DTEND;VALUE=DATE-TIME:20251130T110000Z
UID:109824983925
DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc
 h (Chang Zheng) CZ-7A rocket will launch an unknown payload into orbit.
LOCATION:Pad 201 - Wenchang Satellite Launch Center https://goo.gl/maps/7v
 4maqUT9VigBvQr5
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Ceres 2 • Hongtu
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:272038236186
DESCRIPTION:A Galactic Energy Ceres 2 (Gushenxing 2\, GX-2) rocket will la
 unch on its second? flight\, with ?. The three stage solid-fueled Ceres 2 
 rocket is topped with a liquid-fueled upper stage.
LOCATION:LC-43/95A - Jiuquan Satellite Launch Center https://goo.gl/maps/p
 bNBUb1duneU9V2n6
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Neutron • Test Flight
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:765830501959
DESCRIPTION:A Rocket Lab Neutron rocket will launch on its maiden flight. 
 The methaLOX fueled rocket will feature a reusable first stage powered by 
 nine Archimedes engines and an expendable second stage propelled by an Arc
 himedes vacuum engine.\n-\nDelayed from Q4 2024. Moved forward from early 
 2025. Delayed from late 2024\, mid-2025 and September.\n\nWebcast: \nhttp
 s://www.rocketlabusa.com/live-stream
LOCATION:Neutron Launch Pad\, 41 N Seawall Rd\, Wallops Island\, VA 23337\
 , Vereinigte Staaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC4L • Kuiper
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:185687388747
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated V00?\, wil
 l launch a batch of 45 operational satellites for Amazon's Kuiper constell
 ation. The mission is known as Kuiper ? by ULA and KV-01 by Amazon. The Ce
 ntaur stage will deploy the satellites in an initial orbit of 450km altitu
 de\, the satellites will then use their electric propulsion systems to set
 tle into their assigned final orbits. The Kuiper constellation will enable
  Internet service for customers between 56 degrees north and south latitud
 e. Vulcan will fly in the VC6L vehicle configuration with a double-engine 
 Centaur-LEO upper stage\, six solid rocket boosters and a long fairing.\n-
 \nDelayed from September.
LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\
 , FL 32780\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC4S • USSF-114
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:271726569924
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated ?\, will l
 aunch the USSF-114 mission for the US Space Force. Vulcan will fly in the 
 VC4S? vehicle configuration with a double-engine Centaur upper stage\, fou
 r solid rocket boosters and a standard fairing.\n-\nDelayed from October\,
  Q1 and Q2.
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Gravity YL-2 • Test Flight
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:110432045082
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.
LOCATION:Hainan Commercial Launch Site
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC4S • USSF-87
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:186867392222
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated ?\, will l
 aunch the USSF-87 mission for the US Space Force. It will carry GSSAP 7 an
 d 8 directly into a geosynchronous orbit. This identical pair of Geosynchr
 onous Space Situational Awareness satellites will form part of the USSF’
 s Space Base Situational Awareness (SBSS) constellation\, which tracks spa
 ce traffic and debris in orbit. Vulcan will fly in the VC4S vehicle config
 uration with a double-engine Centaur upper stage\, four solid rocket boost
 ers and a standard fairing.\n-\nDelayed from late 2024\, Q1\, Q2\, August\
 , September and October.
LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\
 , FL 32780\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Hyperbola SQX-3 • Test Flight
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:215948433544
DESCRIPTION:An iSpace (Beijing Interstellar Glory Ltd.) Hyperbola (Shuangq
 uxian\, Shian Quxian) SQX-3 rocket will launch on its first test flight. H
 yperbola 3 is a two-stage\, liquid-fueled\, partially reusable rocket po
 wered by Focus-1 restartable methaLOX engines. The first stage of the roc
 ket is expected to land vertically using landing legs.
LOCATION:Hainan Commercial Launch Site
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC4S • USSF-112
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:351570331251
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated ?\, will l
 aunch the USSF-112 mission for the US Space Force. Vulcan will fly in the 
 VC4S? vehicle configuration with a double-engine Centaur upper stage\, fou
 r solid rocket boosters and a standard fairing.\n-\nDelayed from H2 2024.
LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\
 , FL 32780\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Tianlong TL-3 • TBD
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:312482124547
DESCRIPTION:A Space Pioneer Tianlong 3 rocket will launch on its maiden fl
 ight. It will carry 36 satellites into orbit. The two stage launcher is po
 wered by nine Tianhuo TH-12 keroLOX engines on the first stage and a stage
 d combustion cycle keroLOX engine on the 2nd stage. Tianlong 3 is planned 
 to feature a reusable first stage on later flights.\n-\nDelayed from June\
 , July\, September 2024\, June\, late July and September.
LOCATION:Jiuquan Satellite Launch Center
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Pallas 1 • Test Flight
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:171936431056
DESCRIPTION:A Galactic Energy Pallas 1 (Zhishenxing 1\, 智神星一号\, 
 ZX-1) rocket will launch on its maiden flight to orbit. The two-stage rock
 et uses seven Welkin keroLOX engines on the first stage and one Welkin Vac
  engine on the second stage. The first stage will be developed into a reus
 able booster equipped with grid-fins and landing legs. Galactic Energy (ak
 a Xinghe Power (星河动力) or Beijing Xinghe Dongli Space Technology Co
 . Ltd.) is a Chinese launcher startup.\n-\nDelayed from November 2024\, Au
 gust and October.
LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf
 kosKTdhF5khDg8
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Kinetica 2 • Qingzhou 1
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:218832678026
DESCRIPTION:A CAS Space Kinetica 2 rocket will launch on its first flight.
  The payload will be a prototype of the Cargo Spaceship Qingzhou (轻舟
 一号). It is a single-module cargo spacecraft with 27 cubic meters of sp
 ace\, capable of carrying 1.8 to 2 tonnes of cargo. Total launch mass is 5
  tonnes. The Qingzhou spacecraft adopts an integrated single-cabin configu
 ration design\, which greatly reduces the external dimensions. It is also 
 launcher agnostic. On its first mission Qingzhou will be a free flyer\, t
 he current plan is to dock on the second mission. Kinetica 2 (Lijian 2) w
 as developed by CAS Space (a.k.a. Beijing Zhongke Aerospace Exploration Te
 chnology Co.)\, a spin-off of the Chinese Academy of Sciences. It is equip
 ped with 3 YF-102 keroLOX engines on its first stage and side boosters and
  will be developed into reusability.\n-\nDelayed from August\, September a
 nd November.
LOCATION:LC-43/140 - Jiuquan Satellite Launch Center https://maps.app.goo.
 gl/C5QccUL9HvRGr9629
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Yuanxingzhe 1 • Test Flight
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:268208054127
DESCRIPTION:A Space Epoch (SEPOCH) Yuanxingzhe 1 (元行者一号) rocket 
 will launch on its first test flight\, after a successful suborbital hop a
 nd water landing earlier this year. Yuanxingzhe 1 is a two-stage\, liquid-
 fueled\, partially reusable rocket powered by Longyun-70 (Dragon Cloud) re
 startable methaLOX engines. The first stage of the rocket is expected to 
 land vertically on a sea based platform using landing legs.
LOCATION:TBD
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) RFA One • Test Flight
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:306263062222
DESCRIPTION:Rocket Factory Augsburg will launch a RFA One rocket on its ma
 iden flight from the SaxaVord Spaceport on the Shetland Islands. It will f
 ly a research mission for Ukraine-based Lunar Research Service (LRS) and t
 he PocketQubes ERMINAZ 1U\, ERMINAZ 1V\, MARIA-G (HADES-F)\, QUBIK 5 and U
 NNE 1 (HADES-E). Seven companies had been selected by DLR to launch payloa
 ds aboard the maiden RFA flight\, totaling 136kg. The companies selected w
 ere TU Munich\, SPACEMIND\, Planetary Transportations Systems\, AMSAT-Deut
 schland\, DCUBED\, and Kinetik Space. The three stage launcher is powered 
 by nine keroLOX Helix engines on the first stage and one Helix engine on t
 he second stage. The third stage (named RFA Redshift) is powered by a nitr
 omethane and N2O consuming Fenix engine\, and will also be used as OTV. Ev
 entually the first stage will be reused by parachute-assisted ocean recove
 ry on later flights.\n-\nDelayed from late 2022\, March\, July\, December 
 2023\, May\, August 2024 and summer.
LOCATION:SaxaVord Spaceport\, Unst\, Shetland ZE2 9EF\, Vereinigtes König
 reich
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • RAISE 4
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:241186994482
DESCRIPTION:A Rocket Lab Electron rocket will launch RAISE 4 for JAXA. The
  RAISE 4 (RApid Innovative payload demonstration SatellitE 4) is a platfor
 m for developing small 100kg-class satellites equipped with standard compo
 nents and equipment. The mission was switched from Epsilon S to Electron i
 n 2025. Rocket Lab's mission will be named "RAISE And Shine".
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) SSLV • TBD & CubeSat
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:322945448999
DESCRIPTION:An NSIL SSLV rocket will launch on its first operational fligh
 t\, designated SSLV-L1\, to place an unknown payload into orbit. It will c
 arry an ISRO primary payload and the CubeSat PARIKSHIT.\n-\nDelayed from Q
 4 2024.
LOCATION:Satish Dhawan First Launch Pad\, Sriharikota\, Andhra Pradesh 524
 124\, Indien
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Vulcan VC4S • PWSA
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:170190212753
DESCRIPTION:A United Launch Alliance Vulcan rocket\, designated ?\, will l
 aunch 7 Tranche 1 operational satellites for the U.S. military’s Space 
 Development Agency PWSA (Proliferated Warfighter Space Architecture) const
 ellation. The Tranche 1 satellites (codenamed ?) on this flight are for th
 e Transport Layer and were built by ?. The mission is designated as SDA-T1
 TR-B. Vulcan will fly in the VC4S? vehicle configuration with a double-en
 gine Centaur upper stage\, four solid rocket boosters and a standard fairi
 ng.\n-\nOnce fully operational\, the SDA Tracking Layer will consist of a 
 proliferated heterogeneous constellation of Wide Field of View (WFOV) spac
 e vehicles (SVs) that provide persistent global coverage and custody capab
 ility combined with the Missile Defense Agency (MDA) Hypersonic and Ballis
 tic Tracking Space Sensor (HBTSS) Medium Field of View (MFOV) SVs that pro
 vide precision global access capability. This set of contract awards will 
 initiate the development of the first eight low-cost proliferated WFOV SVs
 . The capability demonstrated by the Tracking Layer Tranche 0 will provide
  missile warning and tracking information to national defense authorities\
 , and tracking and cueing data for missile defense elements. Each satellit
 e will have a “wide field of view” overhead persistent infrared (OPIR)
  sensor capable of detecting and tracking advanced missile threats from lo
 w Earth orbit. The satellites will also be equipped with optical crosslink
 s to pass data to the Transport Layer relay satellites.\nThe first phase o
 f SDA’s Proliferated Warfighter Space Architecture consists of 28 satell
 ites (Tranche 0 including 20 communications payloads made by Lockheed Mart
 in and York 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 t
 o provide an initial operational capability. In total\, Tranche 1 will con
 sist of 154 operational satellites: 126 in the transport layer developed b
 y York\, Northrop Grumman\, and Lockheed Martin\, and 28 focused on missil
 e warning and tracking developed by Northrop Grumman and L3Harris. Combini
 ng conventional tactical radio links\, laser inter-satellite communication
 s\, and wide-view infrared sensors\, hundreds more SDA spacecraft could la
 unch later as the Pentagon ramps up efforts and integrates new capabilitie
 s.\n-\nDelayed from June\, September and October.
LOCATION:Vandenberg AFB Space Launch Complex 3 - East\, Lompoc\, Kaliforni
 en 93436\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) GSLV Mk.II • NavIC 12
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:461502601782
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.\n-\nNVS 3 (NVS-03) is the twelfth satellite in the Navigation 
 with Indian Constellation (NavIC) and the third 2nd generation NavIC satel
 lite. This new series of satellites have a launch mass of 2250kg\, incorpo
 rate L1 band signals additionally to L5 and S-band and use indigenous atom
 ic clocks. The satellite is powered by two solar arrays\, which generate u
 p to 1660 Watts\, and has a lifetime of 12 years.\nThree of the satellites
  in the NavIC constellation are in GEO (Geostationary Orbit) at 32.5°\, 8
 3° and 131.5° East\, while four satellites are in an inclined geosynchro
 nous 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.
LOCATION:Second Launch Complex\, Nellore Dist\, Sriharikota\, Andhra Prade
 sh 524124\, Indien
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Falcon 9 B5 • PWSA
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:144358627433
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 ?) on this flight are for the Transport Layer and were built
  by ?. The mission is designated as SDA-T1TL-D and the Falcon 9 booster is
  B10XX.X for this flight. The 2nd stage is equipped with a Mission Extensi
 on Kit. Comprising a gray band on the RP-1 tank\, extra helium bottles & b
 atteries\, this kit extends the life of the stage in-orbit\, allowing it t
 o deploy the payload directly into its operational orbit.\n-\nOnce fully o
 perational\, the SDA Transport Layer will consist of a proliferated hetero
 geneous constellation of data relay space vehicles (SVs) that provide pers
 istent global coverage through a mesh network comprised of communication s
 atellites that connect to one another and to other space vehicles and grou
 nd stations via optical intersatellite links (OISLs). By nature of the mes
 h network spanning the globe\, the Transport satellites will also be able 
 to transmit precise position\, navigation and timing (PNT) data to enhance
  GPS. A-class satellites have at least four optical cross-links\, that is 
 so they can talk to satellites that are in plane with one another as they'
 re traveling and they also can talk to satellites that are cross-plane or 
 in completely different orbits. So they can maintain those four lines of c
 ommunication simultaneously. The B-class satellites will connect directly 
 to the warfighters via the Link-16 military communications system. They ha
 ve two optical cross-links each\, so that allows them to maintain constant
  communication with the other transport satellites in plane. The two other
  nodes will be Link-16 transmitters. Link-16 is an existing tactical commu
 nication system used across the services primarily for air and ground syst
 ems to share low latency data. The first phase of SDA’s Proliferated War
 fighter Space Architecture consists of 28 satellites (Tranche 0 including 
 20 communications payloads made by Lockheed Martin and York Space\, and ei
 ght missile-tracking infrared sensor satellites made by SpaceX and Leidos)
  as a proof of concept for the missile tracking and data relay network\, f
 ollowed by more than 150 additional satellites to provide an initial opera
 tional capability. In total\, Tranche 1 will consist of 154 operational sa
 tellites: 126 in the transport layer developed by York\, Northrop Grumman\
 , and Lockheed Martin\, and 28 focused on missile warning and tracking dev
 eloped by Northrop Grumman and L3Harris. Combining conventional tactical r
 adio links\, laser inter-satellite communications\, and wide-view infrared
  sensors\, hundreds more SDA spacecraft could launch later as the Pentagon
  ramps up efforts and integrates new capabilities.-\nDelayed from Q4\, Q1 
 and Q3.\n\nWebcast:\nhttps://www.spacex.com/launches\nhttps://spaceflightn
 ow.com
LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343
 6\, USA
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Ariane 62 • Galileo 33–34
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:218392595294
DESCRIPTION:Arianespace will launch an Ariane 6 rocket on a mission design
 ated VA266\, to carry two Galileo-FOC satellites\, designated FM29 & FM30
 \, for Europe’s Galileo navigation constellation into Medium Earth Orbit
  (MEO). They might be the first 2nd gen sats for Galileo\, which feature a
  number of upgrades\, including electric propulsion\, fully digital naviga
 tion payloads\, inter-satellite links\, more powerful navigation antennas\
 , and an advanced atomic clock configuration. Each satellite weighs up to 
 2.4 tonnes\, significantly more than the 700kg 1st gen satellites. Ariane 
 6 will fly in the Ariane 62 configuration\, using 2 solid rocket boosters.
 \n-\nA consortium consisting of OHB-System GmbH and SSTL builds the Galile
 o-FOC (Galileo-Full Operational Capability) satellites. OHB-System acts as
  prime contractor and builds the busses while SSTL provides the payloads. 
 The satellites have a launch mass of 733kg each and carry a navigation pay
 load consisting of two rubidium and two hydrogen maser atomic clocks. The 
 navigation signals are broadcast on L-band. An additional payload is the M
 EO SAR search and rescue transponder payload. The planned service life of 
 each satellite is 12 years or more.\nThe Galileo satellite navigation syst
 em will consist of a total of 30 spacecraft in three planes in medium Eart
 h orbit\, which will each be occupied by nine satellites\, and with three 
 spares satellites distributed on the three orbital planes. At an altitude 
 of 23\,616km and an inclination of 56 degrees\, the system will provide ac
 curate positioning data to users as far north as 75 degrees longitude. In 
 contrast to the American GPS system and the Russian GLONASS navigation net
 work\, Galileo-FOC will be under the control of civilian organisations. Ga
 lileo is the first joint program to be shared between the European Space A
 gency and the European Union.\n\nWebcast:\nhttps://www.arianespace.com/roa
 d-to-space/
LOCATION:ELA4 (l'Ensemble de Lancement Ariane 6) - Centre Spatial Guyanais
 \, 7675+V4M\, Sinnamary 97310\, Französisch-Guyana
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Epsilon S • LOTUSat 1
DTSTART;VALUE=DATE:20251201
DTEND;VALUE=DATE:20251202
UID:133629431366
DESCRIPTION:An IHI Aerospace Epsilon S rocket will launch on its first fli
 ght\, and the seventh flight for the Epsilon launcher overall. Payload is 
 LOTUSat 1.\n-\nDelayed from Q4 2024.
LOCATION:Epsilon Rocket Launch Site\, Minamikata\, Kimotsuki\, Kimotsuki B
 ezirk\, Präfektur Kagoshima 893-1402\, Japan
END:VEVENT
BEGIN:VEVENT
SUMMARY:H3-22S • QZSS 7
DTSTART;VALUE=DATE-TIME:20251207T023000Z
DTEND;VALUE=DATE-TIME:20251207T033000Z
UID:262652913043
DESCRIPTION:A Mitsubishi Heavy Industries H3 rocket will launch the sevent
 h Michibiki (みちびき 5\, QZS 5) navigation satellite for JAXA into ge
 ostationary orbit. The mission is designated as H3F8. Michibiki 5 has a l
 aunch mass of ~4.9 tonnes\, a power generation of 2.7kW and a design life 
 of more than 15 years. The H3 launcher will fly as 22S variant with two m
 ain engines\, two SRB-3 solid strap-on boosters and a short fairing.
LOCATION:Yoshinobu Launch Complex 2 - Tanegashima Space Center\, Japan\, 
 〒891-3703 Kagoshima\, Kumage District\, Minamitane\, Kukinaga\, 麻津
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) Electron • STP-S30
DTSTART;VALUE=DATE:20251208
DTEND;VALUE=DATE:20251209
UID:574342834087
DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w
 ill launch the STP-S30 mission for the US Space Force into orbit. It will 
 carry a batch of four DISKSat prototypes\, based on a new disk shaped flat
 -bed satellite form factor developed by The Aerospace Corporation. Rocket
  Lab has named the mission "?".\n-\nMoved forward from April.\n\nWebcast:
  \nrocketlabusa.com/live-stream\nhttps://spaceflightnow.com
LOCATION:LC2\, 41 N Seawall Rd\, Wallops Island\, VA 23337\, Vereinigte St
 aaten
END:VEVENT
BEGIN:VEVENT
SUMMARY:(NET) LVM3 • SpaceMobile
DTSTART;VALUE=DATE:20251208
DTEND;VALUE=DATE:20251209
UID:200046002620
DESCRIPTION:ISRO’s LVM3 rocket (formerly GSLV Mk.III)\, flying on the LV
 M3-M6 mission\, will launch the first BlueBird Block 2 satellite for AST S
 paceMobile. The satellite is designated as FM1 and has a launch mass of 58
 50kg. The satellites use AST & Science's patented technologies for connect
 ing to cellphones in a space environment for their SpaceMobile constellati
 on.\n-\nThe BlueBird Block 2 satellites are twice as large and have 10 tim
 es the capacity of the Block 1 sats and the BlueWalker 3 prototype. The 
 company needs between 45 and 60 BlueBirds for continuous coverage in the U
 nited States\, supporting text\, voice and data services.\n-\nDelayed from
  May and July.
LOCATION:Second Launch Complex\, Nellore Dist\, P69J+W5X\, Sriharikota\, A
 ndhra Pradesh 524124\, Indien
END:VEVENT
END:VCALENDAR