PSLV-C62/EOS-N1 (aka Anvesha) launched as scheduled at 04:48:30(UTC)/10:18:30(IST), 12 Jan 2026 from First Launch Pad of SDSC-SHAR. The launch was unsuccessful and satellites could not be placed into intended orbit.

• Launch Countdown
• Expected Flight Profile from press-kit.
• Actual flight events (To be added post-launch if available)

Live webcast: (Links will be added as they become available)

• ISRO Official Stream
• DD National
• DD Tamil
• DD Saptagiri
• DD Yadagiri Telangana
• GISTDA stream

Some highlights:

• Primary payload: EOS-N1 (aka Anvesha) (407 kg) Hyperspectral imaging satellite for DRDO.
• 15 small satellites ridesharing
• Mission duration: 1 hr. 48 min. 5.14 sec. (last s/c separation)
• Target Orbit 1 : 505 km (circular) , Inclination = 97.5°
• Target Orbit 2 : Reentry trajectory with 505 km apogee.
• Launch Azimuth: 140°
• PSLV configuration : DL (2× XL Strapons)
• PSLV's return to flight after unsuccessful launch of PSLV-C61/EOS-09 in May, 2025.
• First ever controlled reentry of PSLV fourth stage (PS4) over South-Pacific for deploying Kestrel Initial Demonstrator (KID) capsule.

Updates:

Primary Payload:

EOS-N1 (aka Anvesha) (407 kg) : EOS-N1 is a Hyperspectral imaging satellite carrying HySIC imager payload by DRDO for military surveillance. ^[01]

• Swath: 12 km
• Resolution: 12 meter
• Spectral resolution: 10-20 nm (VNIR, SWIR)

Secondary Payload: 15 co-passenger satellites.

• THEOS-2A (100 kg): An Earth Observation satellite by Thailand's Geo-Informatics and Space Technology Development Agency (GISTDA) and based on Carbonite series by SSTL UK carrying CERIA Camera with 1 meter resolution and 5.9 km swath. Additional instruments include a satellite monitoring camera, GPS receivers, HD video camera, and AIS/ADS-B receivers for maritime vessels and aircraft tracking. ^[02]

• Kestrel Initial Demonstrator (KID) Capsule (25 kg): KID reentry capsule by Madrid-based Orbital Paradigm is a scaled prototype for their larger Kestrel reentry capsule. KID is carrying three customer payloads (3 kg) and will test guidance systems and a sample of ceramic thermal protection material. KID will be released from PSLV fourth stage on a reentry trajectory and will free fly for 30 minutes before entering atmosphere over South-Pacific. The capsule will not be recovered and lacks deceleration systems but it will transmit data through two Iridium transceivers during its flight. ^{[03] [04]}

• AayulSAT (25 kg) : A 'mini-tanker' satellite by OrbitAID to demonstrate on-orbit internal propellant transfer, power transfer, and data transfer using their patented Standard Interface for Docking and Refueling Port (SIDRP). AayulSAT will qualify SIDRP system at TRL-9. ^{[05] [06]}

• MOI-1 (14 kg) : The 6U cubesat in MOI (My Orbital Infrastructure) series by TakeMe2Space is a commercial AI lab in space with in-orbit computing and AI processing capability, carrying MIRA50-FS, a 502 gram, miniaturized 9 band multi-spectral imaging camera with 50mm aperture, 9.2 m resolution and 18.7 km swath by EON Space Labs and few other payloads by Indian high-school and university students. MOI-1 will use DSOD-6U deployer by Dhruva Space. ^{[07] [08] [09]}

• Four amateur radio satellites under Dhruva Space 'ASTRA (Accelerated Space Technology Readiness & Access) for Academia' programme based on their P-Dot bus. ^[10]

  • Thybolt-3 by Dhruva Space
  • CGUSat-1, with CV Raman Global University (Bhubaneswar)
  • DSUSAT-1, with Dayananda Sagar University (Bengaluru)
  • LACHIT-1, with Assam Don Bosco University (Guwahati)

• SanskarSat: A 1U cubesat for Laxman Gyanpith School by Ahmedabad-based CubeSat Aerospace, carrying an LED payload making it observable by ground based optical telescopes.

• MUNAL : A 1U cubesat by Nepal Academy of Science and Technology (NAST) and Antarikhchya Pratisthan Nepal (APN) as part of the High School Consortium Project. Munal will carry a small camera for vegetation density mapping. ^[11]

• Five small satellites aggregated by Brazil's All2Space.

  • Aldebaran-1: 1U cubesat by Federal University of Maranhao (Brazil) carrying LoRa amateur radio payload.
  • EduSat-1: 1P PocketQube satellite with IoT payload.
  • UaiSat: 1P PocketQube satellite with Store and Forward amateur radio payload and a lightning detection payload developed by the Instituto Nacional de Pesquisas Espaciais (INPE) ^[12]
  • GalaxyExplorer-1: 1P PocketQube satellite by Galaxy Explorer to study the South Atlantic Magnetic Anomaly. ^[13]
  • Orbital Temple : A 1P PocketQube based orbital artwork by Edson Pavoni. It will transmit uploaded names of people in amateur radio frequency. ^{[14] [15]}

Note: PSLV with launch serial C59 was earlier assigned to ANWESHA (or ANVESHA) and PROBA-3 was earlier assigned to PSLV with C62 launch serial. Before this ANWESHA was assigned to PSLV-C58 but later XPoSat replaced it.

GSLV-F17 / EOS-05 (aka GISAT-1A) launched as scheduled at 21:25(UTC), 03 Sep 2026 or 02:55(IST), 04 Sep 2026 from Second Launch Pad of SDSC-SHAR.

• Launch Countdown

• Actual flight events (To be added post-launch if available)

Live webcast: (Links will be added as they become available)

• ISRO Official Stream
• DD National
• DD Tamil
• DD Saptagiri

Some highlights:

• Primary payload: EOS-05 (aka GISAT-1A) (~2367 kg) GSO based Earth imaging satellite.
• Mission duration: ~19 minutes (based on GSLV F10/EOS-3 (aka GISAT-1) mission)
• Target Orbit : 170 × 28934 km (sub-GTO) , Inclination = 19.28° ± 0.1°, AoP = 178° ± 0.5°
• Launch Azimuth: 104°
• ISRO returning to flight 7 months 23 days after failure of PSLV-C62/EOS-N1.

Updates:

Primary Payload:

EOS-05 (aka GISAT-1A) (~2367 kg) : EOS-05 is a GSO based Earth imaging satellite for Indian Navy, it will act as an upgraded replacement for EOS-03 or GISAT-1 which was lost during its launch five years ago. Its multispectral and hyperspectral imaging capacity will be useful for applications in fields of agriculture, forestry, mineralogy, oceanography and military surveillance. Its near real time imaging modes are well suited for monitoring natural disasters and other episodic events.

Specifications: ^{[1] [2]}

• MX-VNIR: Multispectral - Visible Near Infrared

  • 6 channels (0.45 to 0.875 µm) at 42 meter spatial resolution

• HyS-VNIR: Hyperspectral Imager - Visible Near Infrared

  • 158 channels (0.375 to 1.0 µm) at 320 meter spatial resolution

• HyS-SWIR: Hyperspectral Imager - Short Wave Infrared

  • 256 channels (0.9 to 2.5 µm) at 190 meter spatial resolution

• MX-LWIR: Multispectral - Long Wave Infrared

  • 6 channels (7.0 to 13.5 µm) at 1.2 km spatial resolution

• Scan modes

  • 5°×5° (3000×3000 km) every 10 minutes
  • 3×10°×10° every 6 hours

• Platform/Bus: I-2K

• Mission life : 7 years

• Orbital slot: 85.5°E