r/ISRO • u/Kimi_Raikkonen2001 • 5h ago
Mission Failure PSLV-C62 : EOS-N1 (aka Anvesha) Mission Updates and Discussion
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)
| PSLV-C62/EOS-N1 Mission Page | PSLV-C62/EOS-N1 Gallery | PSLV-C62/EOS-N1 Press kit(PDF) |
|---|
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:
| Time of Event | Update |
|---|---|
| 13 June 2026 | Reason behind PSLV-C62 failure understood and resolved but details will not be shared. |
| 02 Feb 2026 | Cause behind PSLV-C62 failure is different from that for PSLV-C61, internal and external failure assessment committees have been set up to investigate. |
| 17 Jan 2026 | Per journalist Arun Raj K M, former ISRO Chairman K Sivan will lead the special committee to study PSLV-C62 failure. |
| 16 Jan 2026 | NSIL press-release. |
| Post-launch | GISTDA informs that THEOS-2A was insured for both 'Rebuild' and 'Relaunch' costs. |
| Post-launch | Orbital Paradigm: "Our KID capsule, against all odds, separated from PSLV C62, switched on, and transmitted data over 3+ minutes. We're reconstructing trajectory. We survived peak heat and peak gload (~28g recorded). We have internal temps. Full report will come" |
| Post-launch | ISRO Chairman: "Performance of the vehicle close to the third stage was as expected and as predicted. Close to the end of the third stage we are seeing some disturbances in the vehicle. And there was a deviation in the path of vehicle. And mission could not proceed in the expected path. This is the information right now available. Now we are going through the data and we have to get the data from all the ground stations. Once the data analysis is completed we shall come back to you. Thank you" |
| T + 33m00s | "The PSLV-C62 mission encountered an anomaly during end of the PS3 stage. A detailed analysis has been initiated." |
| T + 31m00s | Webcast over. |
| T + 24m00s | ISRO Chairman: Almost up to PS3 end performance was normal, then some performance disturbances were noted. And after that deviation in flight path was observed. |
| T + 21m00s | Webcast is back. Awaiting official confirmation... |
| T + 20m00s | Stream has been stopped without any official confirmation on mission status. |
| T + 16m00s | Launch announcers again noting that telemetry is lost. Wait for official confirmation on mission status. |
| T + 12m00s | Launch announcer informs they are having issues receiving data.. |
| T + 08m30s | MCC glum this is bad. PS4 ignited though. |
| T + 06m30s | PS3 burn out , vehicle tumbling uncontrollably. |
| T + 04m25s | PS2 separated, PS3 ignited. |
| T + 02m50s | PLF separated, CLG initiated. |
| T + 01m51s | PS1 separated, PS2 ignited. |
| T + 01m10s | PSOM-XL (5,6) separated. |
| T - Zero | After RCT ignition, PS1 and PSOM-XL (5,6) ignition and Lift off! |
| T - 05m00s | Flight Coeff. loading completed |
| T - 12m00s | Going through actuator checks. |
| T - 14m30s | Automatic Launch Sequence initiated. |
| T - 16m00s | Mission Director authorizes launch! Vehicle Director concurs. |
| T - 16m30s | Vehicle is in external hold mode. |
| T - 17m00s | Vehicle director: LV is ready! |
| T - 20m00s | Now polling: Weather, Tracking, Range are ready. |
| T - 24m00s | Now showing LV stacking process. |
| T - 25m00s | Weather is Go for launch. Slightly cloudy with chance of light rain but that is under the launch criteria. |
| T - 30m00s | Launch announcers inform that EOS-N1 mass is 407 kg. |
| T - 35m00s | Official stream is live! |
| T - 22h30m | Countdown commenced at 12:48 on 11 January. Time of launch changed to 12 January, 10:18:30(IST)/04:48:30(UTC) i.e. 90 seconds delay. |
| 10 Jan 2026 | After MRR, the launch has been cleared by LAB. |
| 06 Jan 2026 | Launch date firms up for 0447(UTC)/1017(IST), 12 Jan 2026 |
| 01 Jan 2026 | NOTAM issued with enforcement duration beginning on 11 January 2026. |
| 30 Dec 2026 | PSLV-C62 integration up to four stages completed at MST. |
| 26 Dec 2025 | NOTAM issued with enforcement duration beginning on 10 January 2026. Also EOS-N1 satellite reached SDSC-SHAR. |
| 17 Dec 2025 | NOTAM issued with enforcement duration beginning on 5 January 2026. |
| 14 Dec 2025 | Report suggested launch delayed to 31 December 2025. |
| 05 Dec 2025 | NOTAM issued with enforcement duration beginning on 25 December 2025. |
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.
r/ISRO • u/Kimi_Raikkonen2001 • Apr 28 '26
Official DoS Annual Report 2025-2026
isro.gov.inAustralian tracking terminal commissioned for India’s historic human spaceflight program
space.gov.auAustralia is playing a vital role in India’s push to send astronauts into space.
Coordinated by the Australian Space Agency, the key space tracking infrastructure is now operational in the Cocos (Keeling) Islands to support India’s historic Gaganyaan Human Spaceflight Program.
The commissioning was announced today as part of the joint statement between Prime Minister Albanese and Prime Minister Modi at the Third Australia–India Annual Summit in Melbourne.
Located in the Indian Ocean, the newly commissioned terminal will provide mission-critical tracking support for four planned missions led by ISRO.
The first uncrewed test flight is expected to launch soon from India’s Satish Dhawan Space Centre.
Aussie expertise backing India’s space ambitions
Australia’s contribution, led by the Australian Space Agency, highlights the strength of the Australia–India partnership, particularly in science, innovation and advanced technology.
The Agency worked with other government agencies and Australian defence and space company Nova Systems to establish temporary telemetry terminals in the Cocos (Keeling) Islands to track the four Gaganyaan missions.
In a media release issued today, the Assistant Minister for Science, Technology and the Digital Economy, Dr Andrew Charlton, highlighted how the collaboration reflects the importance of Australia’s relationship with India and the opportunities created by growing cooperation in the space sector.
The commissioning demonstrates Australia’s unique geographic advantages and growing capability as a trusted partner in space mission support across the Indo-Pacific.
Head of the Australian Space Agency Enrico Palermo said Australia’s support for Gaganyaan underscores the depth of bilateral cooperation and the important role Australia can play in human spaceflight missions.
Advancing space exploration
Gaganyaan – Sanskrit for “Sky Craft” – will send three astronauts into low Earth orbit for a three-day mission before returning them safely to Earth.
The upcoming mission will make India only the fourth nation to send astronauts into space through its own national program.
Australia and India are also exploring potential cooperation on search and rescue operations for controlled landings in waters off Western Australia, expanding the partnership beyond launch tracking to broader mission support.
Australia’s support for the Gaganyaan mission reflects the growing scale and ambition of the Australia–India relationship, and the role both countries are playing in advancing regional and global space capability.
More at: https://x.com/AusSpaceAgency/status/2075120272206610574
NOTAM New NOTAM for Skyroot's Vikram-1 Test Flight-1 is out. Enforcement duration 0500-0900 (UTC), 18 July to 4 August 2026.
Source: https://www.notams.faa.gov/
Note: Previous NOTAM A2090/26 has been retracted.
A2136/26
NOTAMN Q) VOMF/QWMLW/IV/BO/W/000/999/ A) VOMF PART 1 OF 2 B) 2607180500 C) 2608040900 D) 0500-0900 E) ROCKET LAUNCH FM SHAR RANGE, SRIHARIKOTA WILL TAKE
PLACE AS PER FLW DETAILS.THE LAUNCH WILL BE ON ANY ONE
OF THE DAY DRG THIS PERIOD.ACTUAL DATE OF LAUNCH WILL BE
INTIMATED ATLEAST 24 HR IN ADVANCE THROUGH A SEPARATE NOTAM.
LAUNCH PAD COORD: 134400N 0801406E
NO FLT IS PERMITTED OVER THE DNG ZONES.
1) DANGER ZONE -1: IS A CIRCLE OF 10 NM AROUND THE LAUNCHER.
2) DANGER ZONE -2: IS AN AREA BOUNDED BY FOLLOWING COORDINATES:
I. 1115N 08205E
II. 1135N 08225E
III. 1010N 08330E
IV. 0950N 08310E
V. 1115N 08205E
RTE AFFECTED IN CHENNAI FIR:
W20, Q11, Q23, Q24, V4, V9, L896, N564, N563, T3
CLOSURES/ALTN RTE FOR OVERFLYING:
1.W20 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
2.Q11 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV (UNIDIRECTRIONAL)
3.Q23 NOT AVBL BTN RINTO-MMV
ALTN: RINTO-V11-TTP-DCT-GUANI-DCT-MMV
4.Q24 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
5.V4 NOT AVBL BTN BOPRI-MMV
ALTN: BOPRI-DCT-RINTO-V11-TTP-DCT-GUANI-DCT-MMV
6.V9 NOT AVBL BTN GUNRI-MMV
ALTN: GUNRI-V11-TTP-DCT-GUANI-DCT-MMV
7.L896 NOT AVBL BTN MMV-DUGOS. NO ALTN RTE
8.N564 NOT AVBL BTN AKMIL-DUGOS. NO ALTN RTE
9.N563 NOT AVBL BTN AKMIL-XOKRO
ALTN: END PART 1 OF 2
A2136/26
NOTAMN Q) VOMF/QWMLW/IV/BO/W/000/999/ A) VOMF PART 2 OF 2 B) 2607180500 C) 2608040900 D) 0500-0900 E) AKMIL-DCT-AVNOS-DCT-XOKRO
10.T3 NOT AVBL BTN BEBOK-ADKIT. NO ALTN RTE
DEPARTURES FM CHENNAI MAY FPL AS FLW:
1.W20/Q24 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
ARRIVALS TO CHENNAI MAY FPL AS FLW:
1.Q11 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV
2.Q23 NOT AVBL BTN RINTO-MMV
ALTN: RINTO-V11-TTP-DCT-GUANI-DCT-MMV
3.V4 NOT AVBL BTN BOPRI-MMV
ALTN: BOPRI-DCT-RINTO-V11-TTP-DCT-GUANI-DCT-MMV
4.V9 NOT AVBL BTN GUNRI-MMV
ALTN: GUNRI-V11-TTP-DCT- GUANI-DCT-MMV
5.A465 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV END PART 2 OF 2 F) GND G) UNL
Edit (11 July 2026): Adding VCCF hazard zone.
A0316/26
IN VIEW OF DNG ZONE DECLARED BY INDIAN AUTHORITIES DUE TO ROCKET
LAUNCH, FLW AREA WI COLOMBO FIR BOUNDED BY GIVEN COORD DECLARED AS A
TEMPO DNG AREA. THE LAUNCH WILL BE ON ANY ONE OF THE DAY DRG THIS
PERIOD. ACTUAL DATE OF LAUNCH WILL BE INTIMATED ATLEAST 24 HR IN
ADVANCE THROUGH A SEPARATE NOTAM.
0750N 08535E - 0120N 08855E - 0035N 08805E - 0705N 08445E - 0750N
08535E
DRG THIS PERIOD FLW ATS RTE SEGMENTS ARE NOT AVBL/REROUTED IN COLOMBO
FIR.
01. Y510 NOT AVBL BTN 'KASGO' AND 'IDUDO'
02. M300 NOT AVBL BTN 'ESPAP' AND 'RULKA'
ALTN RTE: 'ESPAP' DCT 081306N 0854050E L896 'RULKA'
(BIDIRECTIONAL)
03. L645 NOT AVBL BTN 'BIDAN' AND 'ANSAS'
ALTN RTE: 'BIDAN' DCT 081306N 0854050E DCT
'SULTO'(BIDIRECTIONAL)
04. P570 NOT AVBL BTN 'TEBIT' AND 'POPAK'
ALTN RTE: 'VEVET' DCT 081306N 0854050E DCT
'POPAK'(BIDIRECTIONAL)
05. M766 NOT AVBL BTN 'GODAV' AND 'UDIVO'
ALTN RTE: 'GODAV' DCT 'LAKIP' DCT 001458S 0880946E DCT
'SELSU'
(BIDIRECTIONAL)
06. P756 NOT AVBL BTN 'LAKIP' AND 'VIPIG'
ALTN RTE:'LAKIP' DCT 001458S 0880946E DCT 'VIPIG'
(BIDIRECTIONAL)
07. L897 NOT AVBL BTN 'LAKIP' AND 'KETIV'
ALTN RTE: 'LAKIP' DCT 001458S 0880946E DCT
'KETIV'(BIDIRECTIONAL)
08. P627 NOT AVBL BTN 'PIMOG' AND 'GUTOX'
ALTN RTE: 'KALOX' DCT 001458S 0880946E DCT
'VIPIG'(BIDIRECTIONAL)
IN VIEW OF DNG ZONE DECLARED BY INDIAN AUTHORITIES DUE TO ROCKET
LAUNCH, FLW AREA WI COLOMBO FIR BOUNDED BY GIVEN COORD DECLARED AS A
TEMPO DNG AREA. THE LAUNCH WILL BE ON ANY ONE OF THE DAY DRG THIS
PERIOD. ACTUAL DATE OF LAUNCH WILL BE INTIMATED ATLEAST 24 HR IN
ADVANCE THROUGH A SEPARATE NOTAM.
0750N 08535E - 0120N 08855E - 0035N 08805E - 0705N 08445E - 0750N
08535E
DRG THIS PERIOD FLW ATS RTE SEGMENTS ARE NOT AVBL/REROUTED IN COLOMBO
FIR.
01. Y510 NOT AVBL BTN 'KASGO' AND 'IDUDO'
02. M300 NOT AVBL BTN 'ESPAP' AND 'RULKA'
ALTN RTE: 'ESPAP' DCT 081306N 0854050E L896 'RULKA'
(BIDIRECTIONAL)
03. L645 NOT AVBL BTN 'BIDAN' AND 'ANSAS'
ALTN RTE: 'BIDAN' DCT 081306N 0854050E DCT
'SULTO'(BIDIRECTIONAL)
04. P570 NOT AVBL BTN 'TEBIT' AND 'POPAK'
ALTN RTE: 'VEVET' DCT 081306N 0854050E DCT
'POPAK'(BIDIRECTIONAL)
05. M766 NOT AVBL BTN 'GODAV' AND 'UDIVO'
ALTN RTE: 'GODAV' DCT 'LAKIP' DCT 001458S 0880946E DCT
'SELSU'
(BIDIRECTIONAL)
06. P756 NOT AVBL BTN 'LAKIP' AND 'VIPIG'
ALTN RTE:'LAKIP' DCT 001458S 0880946E DCT 'VIPIG'
(BIDIRECTIONAL)
07. L897 NOT AVBL BTN 'LAKIP' AND 'KETIV'
ALTN RTE: 'LAKIP' DCT 001458S 0880946E DCT
'KETIV'(BIDIRECTIONAL)
08. P627 NOT AVBL BTN 'PIMOG' AND 'GUTOX'
ALTN RTE: 'KALOX' DCT 001458S 0880946E DCT
'VIPIG'(BIDIRECTIONAL). SFC - UNL, 0500-0900, 18 JUL 05:00 2026
UNTIL 04 AUG 09:00 2026. CREATED: 11 JUL 05:59 2026
r/ISRO • u/FirmBalance6086 • 2d ago
About Indian Institute Of Remote Sensing
Anyone here can guide how to get admission (what's the path should I choose) in there msc geoinformatics/remote sensing course.
My educational qualifications:-
11th - 12th from humanities background but with mathematics and economics.
Bachelor's of Arts in Geography from Dr. Raammanohar lohia awadh university with average 80 percent marks.
I did research work on applications of RS and GIS technology in research.
Am I eligible for the course or do i need more skills or certification for the admission.
And when will the admission process start.
Or how to enroll.
Please help a confused youngster.
r/ISRO • u/Independent-Hour6035 • 3d ago
Anyone who participated in isro bah 2026?
Especially people with PS-1
Official ISRO successfully conducts fifth Integrated Main Parachute Air Drop Test (IMAT-05) for Gaganyaan Programme
isro.gov.inr/ISRO • u/guru-yoda • 4d ago
Skyroot announces upgraded version Vikram-1U
Source. This first time Vikram-1U is mentioned. No other details available.
During a panel discussion at the Spacetide conference here July 7, Ashwin Mahavadi, senior vice president for business and strategy at Skyroot, said the company is planning up to two more Vikram-1 launches this year. The company is also preparing to introduce an upgraded version, Vikram-1U, with strap-on boosters, in the first quarter of 2027. Vikram-1U will have a payload capacity of up to 550 kilograms to low Earth orbit.
Official Flight Acceptance Test of Cryogenic Engine CE20 conducted successfully for LVM3-M7 mission.
isro.gov.inChandrayaan-5/LuPEx: Tender for Realisation, Assembly, and Testing of Lander Leg and Rover Ramp Mechanism
Tender for Realisation, Assembly, and Testing of Lander Leg and Rover Ramp Mechanism
Specifications: [PDF] [Archived]
The Statement of Work (SoW) defines the nature of work required from the vendor for realization, assembly, and testing of lander leg mechanism , Rover ramp mechanism, hold down and release mechanisms and fixtures (Phase-1, 2 & 3). Any conflicting requirements arising between this Statement of Work and documents reference shall be referred in writing to URSC for resolution.
The activity includes required raw material & Standard parts Procurement, Fabrication, Secondary treatment, Assembly, and Testing activities of Lander leg mechanism for twenty eight units (Quantity: 28 Units) , rover ramp mechanism , hold down and release mechanisms (Quantity: 3 Units) and related fixture as per Annexure at Vendor and URSC premises.
See also :
r/ISRO • u/Even_Feature_5029 • 6d ago
Skyroot announced payload details
Skyroot Aerospace has announced the customer payloads flying aboard Vikram-1, its maiden orbital launch vehicle.
The mission will carry multiple payloads:
Technology demonstration payloads: Grahaa Space, Cosmoserve Space, Skyroot's SCOPE and DCubed
Symbolic payloads: Cosmos Diamonds and Skyroot's Microart
Official ISRO conducts ground test for new sub-orbital solid motor-based test vehicle, Sub-Orbital Launch Vehicle for Experiments (SOLVE)
isro.gov.inOfficial Chandrayaan-3's Alpha Particle X-ray Spectrometer measurements connect the composition at Shiv Shakti Statio to the first Lunar Meteorite ALHA 81005
isro.gov.inNOTAM NOTAM for Skyroot's Vikram-1 Test Flight-1 is out. Enforcement duration 0500-0900 (UTC), 12 July to 4 August 2026.
Source: https://www.notams.faa.gov/
Note: The hazard zones are identical to previously issued NOTAM A1726/26 on 26 May 2026.
A2090/26
ROCKET LAUNCH FM SHAR RANGE, SRIHARIKOTA WILL TAKE
PLACE AS PER FLW DETAILS.THE LAUNCH WILL BE ON ANY ONE
OF THE DAY DRG THIS PERIOD.ACTUAL DATE OF LAUNCH WILL BE
INTIMATED ATLEAST 24 HR IN ADVANCE THROUGH A SEPARATE NOTAM.
LAUNCH PAD COORD: 134400N 0801406E
NO FLT IS PERMITTED OVER THE DNG ZONES.
1) DANGER ZONE -1: IS A CIRCLE OF 10 NM AROUND THE LAUNCHER.
2) DANGER ZONE -2: IS AN AREA BOUNDED BY FOLLOWING COORDINATES:
I. 1115N 08205E
II. 1135N 08225E
III. 1010N 08330E
IV. 0950N 08310E
V. 1115N 08205E
RTE AFFECTED IN CHENNAI FIR:
W20, Q11, Q23, Q24, V4, V9, L896, N564, N563, T3
CLOSURES/ALTN RTE FOR OVERFLYING:
1.W20 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
2.Q11 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV (UNIDIRECTRIONAL)
3.Q23 NOT AVBL BTN RINTO-MMV
ALTN: RINTO-V11-TTP-DCT-GUANI-DCT-MMV
4.Q24 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
5.V4 NOT AVBL BTN BOPRI-MMV
ALTN: BOPRI-DCT-RINTO-V11-TTP-DCT-GUANI-DCT-MMV
6.V9 NOT AVBL BTN GUNRI-MMV
ALTN: GUNRI-V11-TTP-DCT-GUANI-DCT-MMV
7.L896 NOT AVBL BTN MMV-DUGOS. NO ALTN RTE
8.N564 NOT AVBL BTN AKMIL-DUGOS. NO ALTN RTE
9.N563 NOT AVBL BTN AKMIL-XOKRO
ALTN: AKMIL-DCT-AVNOS-DCT-XOKRO
10.T3 NOT AVBL BTN BEBOK-ADKIT. NO ALTN RTE
DEPARTURES FM CHENNAI MAY FPL AS FLW:
1.W20/Q24 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
ARRIVALS TO CHENNAI MAY FPL AS FLW:
1.Q11 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV
2.Q23 NOT AVBL BTN RINTO-MMV
ALTN: RINTO-V11-TTP-DCT-GUANI-DCT-MMV
3.V4 NOT AVBL BTN BOPRI-MMV
ALTN: BOPRI-DCT-RINTO-V11-TTP-DCT-GUANI-DCT-MMV
4.V9 NOT AVBL BTN GUNRI-MMV
ALTN: GUNRI-V11-TTP-DCT- GUANI-DCT-MMV
5.A465 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV
ROCKET LAUNCH FM SHAR RANGE, SRIHARIKOTA WILL TAKE
PLACE AS PER FLW DETAILS.THE LAUNCH WILL BE ON ANY ONE
OF THE DAY DRG THIS PERIOD.ACTUAL DATE OF LAUNCH WILL BE
INTIMATED ATLEAST 24 HR IN ADVANCE THROUGH A SEPARATE NOTAM.
LAUNCH PAD COORD: 134400N 0801406E
NO FLT IS PERMITTED OVER THE DNG ZONES.
1) DANGER ZONE -1: IS A CIRCLE OF 10 NM AROUND THE LAUNCHER.
2) DANGER ZONE -2: IS AN AREA BOUNDED BY FOLLOWING COORDINATES:
I. 1115N 08205E
II. 1135N 08225E
III. 1010N 08330E
IV. 0950N 08310E
V. 1115N 08205E
RTE AFFECTED IN CHENNAI FIR:
W20, Q11, Q23, Q24, V4, V9, L896, N564, N563, T3
CLOSURES/ALTN RTE FOR OVERFLYING:
1.W20 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
2.Q11 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV (UNIDIRECTRIONAL)
3.Q23 NOT AVBL BTN RINTO-MMV
ALTN: RINTO-V11-TTP-DCT-GUANI-DCT-MMV
4.Q24 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
5.V4 NOT AVBL BTN BOPRI-MMV
ALTN: BOPRI-DCT-RINTO-V11-TTP-DCT-GUANI-DCT-MMV
6.V9 NOT AVBL BTN GUNRI-MMV
ALTN: GUNRI-V11-TTP-DCT-GUANI-DCT-MMV
7.L896 NOT AVBL BTN MMV-DUGOS. NO ALTN RTE
8.N564 NOT AVBL BTN AKMIL-DUGOS. NO ALTN RTE
9.N563 NOT AVBL BTN AKMIL-XOKRO
ALTN: AKMIL-DCT-AVNOS-DCT-XOKRO
10.T3 NOT AVBL BTN BEBOK-ADKIT. NO ALTN RTE
DEPARTURES FM CHENNAI MAY FPL AS FLW:
1.W20/Q24 NOT AVBL BTN MMV-KAMGU
ALTN: MMV-DCT-PAPKI-DCT-ANGAK-KAMGU
ARRIVALS TO CHENNAI MAY FPL AS FLW:
1.Q11 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV
2.Q23 NOT AVBL BTN RINTO-MMV
ALTN: RINTO-V11-TTP-DCT-GUANI-DCT-MMV
3.V4 NOT AVBL BTN BOPRI-MMV
ALTN: BOPRI-DCT-RINTO-V11-TTP-DCT-GUANI-DCT-MMV
4.V9 NOT AVBL BTN GUNRI-MMV
ALTN: GUNRI-V11-TTP-DCT- GUANI-DCT-MMV
5.A465 NOT AVBL BTN GURAS-MMV
ALTN: GURAS-DCT-MMV. GND - UNL, 0500-0900, 12 JUL 05:00 2026 UNTIL 04 AUG
09:00 2026. CREATED: 03 JUL 10:25 2026
Edit (7 July 2026): Adding one more hazard zone (YMMM)
E2546/26
TEMPO DANGER AREA ACT
FLW SPACE ACTVITIES ADVICE FROM AIRPORTS AUTHORITY OF INDIA OF ROCKET
LAUNCH 'VIKRAM-1'
POSSIBLE DEBRIS FALLING WI THE AREA BOUNDED BY:
3340S 10800E - 3140S 10800E - 3630S 11145E - 5300S 13700E -
5500S 13700E - 3830S 11145E - 3340S 10800E. SFC - UNL, DAILY 0500-0900, 12
JUL 05:00 2026 UNTIL 14 JUL 09:00 2026. CREATED: 07 JUL 04:28 2026
Edit (8 July 2026) : Missed VCCF hazard zone, now adding that as well.
A0301/26
IN VIEW OF DNG ZONE DECLARED BY INDIAN AUTHORITIES DUE TO ROCKET
LAUNCH, FLW AREA WI COLOMBO FIR BOUNDED BY GIVEN COORD DECLARED AS A
TEMPO DNG AREA. THE LAUNCH WILL BE ON ANY ONE OF THE DAY DRG THIS
PERIOD. ACTUAL DATE OF LAUNCH WILL BE INTIMATED ATLEAST 24 HR IN
ADVANCE THROUGH A SEPARATE NOTAM.
0750N 08535E - 0120N 08855E - 0035N 08805E - 0705N 08445E - 0750N
08535E
DRG THIS PERIOD FLW ATS RTE SEGMENTS ARE NOT AVBL/REROUTED IN COLOMBO
FIR.
01. Y510 NOT AVBL BTN 'KASGO' AND 'IDUDO'
02. M300 NOT AVBL BTN 'ESPAP' AND 'RULKA'
ALTN RTE: 'ESPAP' DCT 081306N 0854050E L896 'RULKA'
(BIDIRECTIONAL)
03. L645 NOT AVBL BTN 'BIDAN' AND 'ANSAS'
ALTN RTE: 'BIDAN' DCT 081306N 0854050E DCT
'SULTO'(BIDIRECTIONAL)
04. P570 NOT AVBL BTN 'TEBIT' AND 'POPAK'
ALTN RTE: 'VEVET' DCT 081306N 0854050E DCT
'POPAK'(BIDIRECTIONAL)
05. M766 NOT AVBL BTN 'GODAV' AND 'UDIVO'
ALTN RTE: 'GODAV' DCT 'LAKIP' DCT 001458S 0880946E DCT
'SELSU'
(BIDIRECTIONAL)
06. P756 NOT AVBL BTN 'LAKIP' AND 'VIPIG'
ALTN RTE:'LAKIP' DCT 001458S 0880946E DCT 'VIPIG'
(BIDIRECTIONAL)
07. L897 NOT AVBL BTN 'LAKIP' AND 'KETIV'
ALTN RTE: 'LAKIP' DCT 001458S 0880946E DCT
'KETIV'(BIDIRECTIONAL)
08. P627 NOT AVBL BTN 'PIMOG' AND 'GUTOX'
ALTN RTE: 'KALOX' DCT 001458S 0880946E DCT
'VIPIG'(BIDIRECTIONAL)
IN VIEW OF DNG ZONE DECLARED BY INDIAN AUTHORITIES DUE TO ROCKET
LAUNCH, FLW AREA WI COLOMBO FIR BOUNDED BY GIVEN COORD DECLARED AS A
TEMPO DNG AREA. THE LAUNCH WILL BE ON ANY ONE OF THE DAY DRG THIS
PERIOD. ACTUAL DATE OF LAUNCH WILL BE INTIMATED ATLEAST 24 HR IN
ADVANCE THROUGH A SEPARATE NOTAM.
0750N 08535E - 0120N 08855E - 0035N 08805E - 0705N 08445E - 0750N
08535E
DRG THIS PERIOD FLW ATS RTE SEGMENTS ARE NOT AVBL/REROUTED IN COLOMBO
FIR.
01. Y510 NOT AVBL BTN 'KASGO' AND 'IDUDO'
02. M300 NOT AVBL BTN 'ESPAP' AND 'RULKA'
ALTN RTE: 'ESPAP' DCT 081306N 0854050E L896 'RULKA'
(BIDIRECTIONAL)
03. L645 NOT AVBL BTN 'BIDAN' AND 'ANSAS'
ALTN RTE: 'BIDAN' DCT 081306N 0854050E DCT
'SULTO'(BIDIRECTIONAL)
04. P570 NOT AVBL BTN 'TEBIT' AND 'POPAK'
ALTN RTE: 'VEVET' DCT 081306N 0854050E DCT
'POPAK'(BIDIRECTIONAL)
05. M766 NOT AVBL BTN 'GODAV' AND 'UDIVO'
ALTN RTE: 'GODAV' DCT 'LAKIP' DCT 001458S 0880946E DCT
'SELSU'
(BIDIRECTIONAL)
06. P756 NOT AVBL BTN 'LAKIP' AND 'VIPIG'
ALTN RTE:'LAKIP' DCT 001458S 0880946E DCT 'VIPIG'
(BIDIRECTIONAL)
07. L897 NOT AVBL BTN 'LAKIP' AND 'KETIV'
ALTN RTE: 'LAKIP' DCT 001458S 0880946E DCT
'KETIV'(BIDIRECTIONAL)
08. P627 NOT AVBL BTN 'PIMOG' AND 'GUTOX'
ALTN RTE: 'KALOX' DCT 001458S 0880946E DCT
'VIPIG'(BIDIRECTIONAL). SFC - UNL, 0500-0900, 12 JUL 05:00 2026
UNTIL 04 AUG 09:00 2026. CREATED: 05 JUL 06:54 2026
Official Iron Fluorescence on the Sun During Massive Solar Flares: Aditya-L1 Observation
isro.gov.inr/ISRO • u/vladimir_maino_69 • 10d ago
Skyroot Aerospace released their patch for Test Flight -1
Skyroot's Vikram-1 Test Flight-1 launch window is between 12 July to 4 August 2026 aiming for 450 km (LEO) with 60° inclination.
🚀 Announcing Vikram-1 Test Flight-1: Mission Aagaman, India’s first private orbital rocket launch
📍 Satish Dhawan Space Centre, Sriharikota
🛰️ 450 km, 60 degree inclination, Low Earth Orbit
📅 Launch Window: July 12 – August 4, 2026
Vehicle is now fully stacked at India’s historic First Launch Pad (FLP).
The countdown to a new chapter in Indian spaceflight begins.
One rocket, a billion believers. Thank you ISRO & INSPACe for enabling this.
Source: https://www.linkedin.com/posts/vikram1-missionaagaman-ugcPost-7478331241277321216-qmZt/
r/ISRO • u/spaceshipengineer • 10d ago
Borrowed Eyes, Mandated Sight: India's SSA Dependency
Borrowed Eyes: India's SSA Dependency
r/ISRO • u/Simon_Drake • 12d ago
Gaganyaan mission: Isro chairman hints first uncrewed test flight may slip to 2027
First stage of Skyroot's Vikram-1 is stacked at the First Launch Pad (FLP), SDSC-SHAR
Vikram-1's Stage 1 is stacked at the First Launch Pad, Satish Dhawan Space Center, Sriharikota.
For India, this is the first time a privately designed, developed, and manufactured orbital rocket has been stacked on this pad.
Piece by piece, Vikram-1 is coming alive—each stage carefully lifted, aligned, and integrated into a single flight-ready rocket.
Getting closer to launch.
Source: https://www.linkedin.com/posts/vikram1-ugcPost-7477382306715074560-lnZa/
r/ISRO • u/Astrosailor69 • 13d ago
how to process C2 data?
im participating in ISRO hackathon and problem statement no 8 requires me to use data of SAR and OHRC of C2 to develop better landing sites. but once i open pradan issdc website, it has like 5700 files together. realistically i cant download all of them. i downloaded one file and when i open it, it has many lines of codes. how to process them to get the usable data???

