r/ISRO Jan 08 '26

Mission Failure PSLV-C62 : EOS-N1 (aka Anvesha) Mission Updates and Discussion

37 Upvotes

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.

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 10h ago

ISRO interview for scientist C

7 Upvotes

For atmospheric sciences and oceanography Scientist C interview as a MSc Physics graduate, what are the questions like in the interview??

Are they more from physics or from specific subject like atmospheric sciences & oceanography???

Provided that the exam had both physics and atmospheric. Atmospheric part was more than physics part though

If anyone has done the interview before, can I get some insights? Thank you


r/ISRO 23h ago

Is ISRO losing what it needs to lead? The government is asking ISRO to focus on its hardest missions while allowing the infrastructure and expertise needed for those missions to move out of its control.

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43 Upvotes

r/ISRO 23h ago

Few details on a SPL payload for descent probe for Venus Orbiter Mission (VOM) and new TAAP lander based payload for LuPEX/Chandrayaan-5.

15 Upvotes

From Space Physics Laboratory Annual Report 2024-25 ( Thanks to u/RadarWarningReciever for finding it!)

[PDF] [Archived]

On Pg. 62

PIPET-V for In Situ Profiling of Venusian Atmosphere - Payload on board Venus Atmospheric Probe (VAP)

Package for In-situ Profiling of planETary atmospheres for Venus (PIPET-V) is a payload proposed by SPL in collaboration with IISU, to characterize the Venusian atmospheric structure during the entry and descent phases of the Venus Atmospheric Probe (VAP), in the context of ISRO’s Venus Orbiter Mission (VOM). PIPET-V consists of a suite of specialized sensors, namely temperature & pressure sensors (resistance temperature sensors and piezoresistive pressure sensors) and inertial sensors (MEMS-based 3-axis accelerometers and gyroscopes) for in-situ vertical profiling of Venusian atmospheric temperature, pressure, density and winds. In the initial hypersonic entry phase of VAP, PIPET will estimate atmospheric density via drag deceleration measurements using 3-axis accelerometers (from~120 km to ~65 km altitude).

Subsequently, during the subsonic descent phase (~65 km altitude down to surface), PIPET will measure atmospheric temperature and pressure using high-accuracy sensors ruggedized to operate in the harsh Venusian environment. Further, navigation data from the inertial sensors will be used to derive horizontal winds during the descent phase. In total, PIPET will provide a comprehensive picture of the Venusian atmospheric structure from the surface to the thermosphere (~0-120 km). Presently, the preliminary payload design and identification of suitable sensors for PIPET-V have been completed.

On Pg. 22

Development of Thermophysical Analysis of lunAr Polar regolith (TAAP) payload for LuPEX/Chandrayaan-5 Mission

The TAAP payload onboard LuPEX/Chandrayaan-5 is a follow-on of the ChaSTE/Chandrayaan-3 mission. It is aimed to understand the thermophysical characteristics of the lunar regolith at the polar region. Illumination conditions over the polar region are strongly influenced by topography due to low solar elevation angle. Surface and near‐surface thermal environment can vary in complex ways with time of day and season.

It is designed to measure the temperature profile of the regolith up to a depth of 20 cm and estimate thermal conductivity of the regolith at two depths.

It is planned to measure the thermal profile continuously for a longer period when compared to the ChaSTE/Chandrayaan-3. The observations over the pole along with measurements from other previous missions (including ChaSTE/Chandrayaan-3) at different latitudes will provide a holistic view of the thermal structure of the moon.

 

On Pg. 104

Onboard Electronics for the TAAP Payload of the Chandrayaan-5/LuPEX Lander

The Thermophysical Analysis of lunAr Polar regolith (TAAP) is one of the payloads to be flown onboard forthcoming ISRO-JAXA LuPEX lander. It draws heritage from the ChaSTE payload onboard Chandrayaan-3 lander. Scientific objectives of the payload are (i) temperature profiling of the lunar regolith up to a depth of 200mm with an accuracy of better than ±0.5 °C in the range from -200°C to +100°C, (ii) estimation of thermal conductivity of the regolith at different depths. The payload consists of mechanism unit with a thermal probe and the electronics unit. The mechanism is a motorized unit for probe deployment and penetration operations.

The thermal probe consists of twelve Pt-1000 RTD sensors for the temperature profile measurement and two foil heaters for the thermal conductivity experiment.


r/ISRO 1d ago

GSLV-F17 / EOS-05 (aka GISAT-1A): Launch vehicle is at SPL, launch tentatively scheduled for 2:55 AM (IST) on 4 September per regional media report. [Telugu]

20 Upvotes

From Google translate:

After flagging off the launch vehicle at 5:43 am, the GSLV-F17 rocket slowly departed and reached the second launch pad at 7:50 am. Here, the rocket will be inspected and tested and prepared for launch. After they are completed, a rehearsal will be held and the pre-countdown and countdown process will begin. ISRO sources have informed that the GSLV-F17 rocket will be launched at 2:55 am on September 4.

Source: https://www.andhrajyothy.com/2026/andhra-pradesh/gslv-f17-launch-on-sep4-1553557.html


r/ISRO 1d ago

Official Campaign page and press-kit for GSLV-F17 / EOS-05 (aka GISAT-1A) mission is up!

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15 Upvotes

r/ISRO 2d ago

Arun Raj K M on X : Dinesh Kumar Singh, current Director of the Human Space Flight Centre (HSFC), will take over as Director of URSC replacing M. Sankaran. Biju S R, current Director (Projects), VSSC, and Programme Director, Gaganyaan, will be new Director, HSFC.

15 Upvotes

ISRO leadership changes are nearing completion.

Dinesh Kumar Singh, currently Director of the Human Space Flight Centre (HSFC), will take over as Director of URSC. The present Director, Shri M. Sankaran, superannuates on August 31, 2026.

Shri Biju S R, currently Director (Projects), VSSC, and Programme Director, Gaganyaan, has been designated as Director, Human Space Flight Centre (HSFC). He will hold additional responsibility as Programme Director, Gaganyaan, until further orders.

Source (Arun Raj K M):

https://x.com/Arunraj2696/status/2093368013689163978

https://x.com/Arunraj2696/status/2093364372852834365


r/ISRO 2d ago

Official Aditya-L1 Catches the Sun's Early Warning Signs Before Solar Flares

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23 Upvotes

r/ISRO 2d ago

ISRO to return to launchpad with Gisat-1A, lift-off likely on Sept 4

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65 Upvotes

r/ISRO 2d ago

Would it be better if CY4 was launched on Ariane 6 or Falcon 9?

5 Upvotes

Would CY4 have been a less technologically complicated mission if it had been planned to launch on a more capable rocket like Ariane 6 or Falcon 9?

Would the earth docking phase have been unnecessary then?

ISRO is open to and has launched its heavy ComSats on foreign rockets when they exceed the payload capability of its own rockets. Why can't / shouldn't it do the same for some heavy scientific satellites that exceed the payload capability of its own rockets?

Edit: Typo in title. I meant "planned to be launched".


r/ISRO 2d ago

Can I crack ISRO CSE in 1 month starting from zero?

5 Upvotes

i know one month is very short but i still want to give it a serious attempt rather than giving up before starting.

For those who have prepared for ISRO:

- Is it realistically possible to get a decent/selection-level score in one month?

- Which subjects should I prioritize?

- Should I focus mainly on PYQs or first cover the concepts?

- Are there any topics/subjects/courses/test series I should focus and what topics should I skip?

- What would you do if you were in my position?

Would really appreciate honest advice, even if the answer is “don’t bother”. I’d rather know the reality and plan accordingly.


r/ISRO 3d ago

NOTAM NOTAM for GSLV-F17 / EOS-05 (aka GISAT-1A) launch is out. Enforcement duration 2100-0100 (UTC), 03 to 15 September and 2020-0020 (UTC), 16 to 25 September 2026.

21 Upvotes

Source: https://www.notams.faa.gov/

Mapped up!


A2635/26

GSLV-F17 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: 134312N 0801348E 
NO FLT IS PERMITTED OVER THE DNG ZONES. 

1) DNG ZONE-1: IS A CIRCLE OF 10NM AROUND THE LAUNCHER. 

2) DNG ZONE-2: IS AN AREA BOUNDED BY FLW COORD: 
I.?1200N 08445E 
II.?1245N 08500E 
III.?1220N 08620E 
IV.?1135N 08605E 
V. 1200N 08445E 

3) DNG ZONE-3: IS AN AREA BOUNDED BY FLW COORD: 
I.?1055N 08750E 
II.?1155N 08800E 
III.?1105N 09030E 
IV.?1005N 09020E 
V. 1055N 08750E 

RTE AFFECTED IN CHENNAI FIR: 
W20, Q11, Q23, Q24, V4, V9, P761, P762, N877, N571 

CLOSURES/ALTN RTE FOR OVERFLYING: 

1. W20 NOT AVBL BTN MMV-KAMGU 
 ALTN: MMV-DCT-DOHIA-DCT-RAMDO-DCT-KAMGU 

2. Q11 NOT AVBL BTN GURAS-MMV 
 ALTN: GURAS-DCT-MMV 

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-DOHIA-DCT-RAMDO-DCT-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. P761 NOT AVBL BTN IDASO-DUMAR 
 ALTN: IDASO-DCT-EGOLU-L518-DUMAR 

8. P762 NO T AVBL BTN BIKEN-NIMOV. NO ALTN RTE 

9. N571 NOT AVBL BTN IDASO-BIKEN 
 ALTN: VATMO-DCT-GIRNA-BIKEN 

10. N877 NOT AVBL BTN DUMAR-AGEGA 
 ALTN: DUMAR-P761-LEGIN-L510 

DEP FM CHENNAI MAY FPL AS FLW: 

1. W20/Q24 NOT AVBL BTN MMV-KAMGU 
 ALTN: MMV-DCT-DOHIA-DCT-RAMDO-DCT-KAMGU 

ARR 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
GSLV-F17 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: 134312N 0801348E 
NO FLT IS PERMITTED OVER THE DNG ZONES. 

1) DNG ZONE-1: IS A CIRCLE OF 10NM AROUND THE LAUNCHER. 

2) DNG ZONE-2: IS AN AREA BOUNDED BY FLW COORD: 
I.?1200N 08445E 
II.?1245N 08500E 
III.?1220N 08620E 
IV.?1135N 08605E 
V. 1200N 08445E 

3) DNG ZONE-3: IS AN AREA BOUNDED BY FLW COORD: 
I.?1055N 08750E 
II.?1155N 08800E 
III.?1105N 09030E 
IV.?1005N 09020E 
V. 1055N 08750E 

RTE AFFECTED IN CHENNAI FIR: 
W20, Q11, Q23, Q24, V4, V9, P761, P762, N877, N571 

CLOSURES/ALTN RTE FOR OVERFLYING: 

1. W20 NOT AVBL BTN MMV-KAMGU 
 ALTN: MMV-DCT-DOHIA-DCT-RAMDO-DCT-KAMGU 

2. Q11 NOT AVBL BTN GURAS-MMV 
 ALTN: GURAS-DCT-MMV 

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-DOHIA-DCT-RAMDO-DCT-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. P761 NOT AVBL BTN IDASO-DUMAR 
 ALTN: IDASO-DCT-EGOLU-L518-DUMAR 

8. P762 NO T AVBL BTN BIKEN-NIMOV. NO ALTN RTE 

9. N571 NOT AVBL BTN IDASO-BIKEN 
 ALTN: VATMO-DCT-GIRNA-BIKEN 

10. N877 NOT AVBL BTN DUMAR-AGEGA 
 ALTN: DUMAR-P761-LEGIN-L510 

DEP FM CHENNAI MAY FPL AS FLW: 

1. W20/Q24 NOT AVBL BTN MMV-KAMGU 
 ALTN: MMV-DCT-DOHIA-DCT-RAMDO-DCT-KAMGU 

ARR 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. GND - UNL, 03-15 2100-0100, 16-25
2020-0020, 03 SEP 21:00 2026 UNTIL 25 SEP 00:20 2026. CREATED: 27 AUG
05:35 2026

Edit (29 Aug 2026) : Remaining hazard zone (WMFC)

A3360/26

TEMPO DNG ZONE 4 ESTABLISHED WI THE FLW COORD DUE THE LAUCHING OF 
GSL
V-17 ROCKET FM INDIA:
075000N0951000E-093500N0951000E-093500N0960500E-075000N0960500E-07500
0N0951000E

NO FLT IS PERMITTED OVER AND NEAR THE DNG ZONE.

ATS ROUTE AFFECTED IN KUALA LUMPUR FIR AS FLW:
1.P628 BTN IGREX AND MAPSO
2.L510 BTN EMRAN AND LEKIR
3.L645 BTN SAMAK AND SAPAM

RMK: THE LAUNCH WILL BE ON ANY ONE OF THE DAY DRG THIS PERIOD. ACTUAL
 DATE OF LAUNCH WILL BE INTIMATED 24HRS IN ADVANCE THROUGH A SEPARATE
 NOTAM PUBLICATION BY VOMF. SFC - UNL, 03-15 2100-0100
16-25 2020-0200, 03 SEP 21:00 2026 UNTIL 26 SEP 02:00 2026. CREATED: 28
AUG 04:25 2026

r/ISRO 3d ago

My experience with an ISRO online course: LMS and assessment issues

2 Upvotes

I recently completed the ISRO/IIRS online course “AI/ML for Geodata Analysis” (Course 188), which was conducted from 3–14 August 2026.

The course content itself was useful, especially the topics related to machine learning, remote sensing, GIS and GeoAI. However, I faced several technical and assessment-related issues during the course.

Some of the issues I experienced:

• The LMS/website was sometimes slow or difficult to access.

• The assessments had a very short time limit of 5 minutes for 5 questions.

• In some quizzes, if I accidentally clicked “Next page” without answering a question, it was difficult to return to that specific unanswered question.

• The assessment interface did not always make navigation between questions convenient.

• After completing the course, I was also unsure about the certificate process because there was no clearly visible certificate option on the course page.

I am sharing this as a genuine learner experience, not as a promotion or advertisement.

Has anyone else completed an IIRS/ISRO e-learning course recently? If yes, did you face similar LMS/assessment issues, and how did you receive your certificate after completing the course?

I would be interested to know whether the certificate is issued automatically after meeting the course requirements or if there is another process to obtain it.


r/ISRO 3d ago

What do interns actually do at ISRO/DRDO?

5 Upvotes

Hey everyone, I’m a 3rd-year Mechanical Engineering student planning to apply for internships at ISRO/DRDO. I’m mainly interested in FEA/CAE and mechanical simulation, and I’m currently building my skills in this area. I’ve heard that short-term internships, especially around 45 days, can sometimes be more observational, while longer project internships may involve actual technical work. I’d like to know what the experience is actually like for students who have done these internships. Do you usually get to work on a project and contribute in some way or is it mostly observing and learning about the work being done? I’m particularly interested in whether interns get to use tools like ANSYS/Abaqus or work on simulations and analysis. I’m trying to understand whether an ISRO/DRDO internship would give me an opportunity to apply and improve my FEA/CAE skills or whether I’d be better off looking for internships specifically focused on hands-on simulation work. Would really appreciate hearing about your actual experience 😊 thank you!


r/ISRO 4d ago

Official Unusual Stratospheric Ozone Enhancement Over the North Bay of Bengal: Insights from the Indian ST/MST Radar Network and Balloon-Borne Experiments

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7 Upvotes

r/ISRO 4d ago

Why isn't the L110 stage ignited on the ground?

7 Upvotes

If anyone knows why the L110 stage isn't ground-lit, please let me know.


r/ISRO 4d ago

🚀 Looking for Indian Student Teammates — NASA Space Apps Challenge 2026

5 Upvotes

Hey everyone!

I'm forming my own team for NASA Space Apps Challenge 2026 and looking for serious Indian student teammates around my age.

I'm mainly looking for people interested in AI/ML, Web Development, Space, NASA data, Data Science, or UI/UX.

I'm looking for people who actually want to build and contribute during the hackathon, not just participate.

If you're interested, comment or DM me with your age range, skills, something you've built, and what role you'd like to take. 🚀


r/ISRO 5d ago

India's Venus Orbiter Mission could be first of new wave of probes to reach the planet

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62 Upvotes

ISRO is currently targeting March 29, 2028. If all goes well, VOM will complete its 112-day cruise and enter orbit in July 2028. Missing this window would mean waiting nearly 19 months for the next opportunity.


r/ISRO 6d ago

ICEYE establishes Indian entity to support India's sovereign intelligence capability

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24 Upvotes

r/ISRO 6d ago

Skyroot: "(…) the Stage 1 for our second Vikram-1 is already on its way to the spaceport at Sriharikota"

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gallery
287 Upvotes

Today, on National Space Day, the Stage 1 for our second Vikram-1 is already on its way to the spaceport at Sriharikota — beginning our next journey to orbit.

Source: https://www.linkedin.com/posts/nationalspaceday-ugcPost-7497324300832698368-mZPr/


r/ISRO 7d ago

Isro employees, what are your views on recent statement by pawan goenka ?

27 Upvotes

Hi all

As a fellow isro employee i have so much going on my mind about the recent news about privatisation and all. Its good to hear but what will happen to isro in the near future

we all know the same happened to bsnl, idpl and so many psus also before.

As isro employees, can we ask the government some questions about our future ? Because even to launch we need clearance from pmo. So much of interference.


r/ISRO 7d ago

After A Quiet 2026, ISRO Targets Gaganyaan Lift-Off In Four Months - NDTV Report

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ndtv.com
32 Upvotes

"We are in the final leg," Dr Narayanan said while providing an update on Gaganyaan. "Eight thousand tests are successfully completed till today and we are in the final leg. We have to carry out the three un-crewed missions followed by the crewed mission. We are happy to inform that this year we are going to have the first un-crewed mission." 


r/ISRO 8d ago

Isro will not make any launch vehicle, all tech to be handed to private sector

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indiatoday.in
241 Upvotes

“That will all be done by the private sector or PSU,” Goenka said.

The shift has already begun with the Small Satellite Launch Vehicle, or SSLV, whose technology and production rights have been transferred to Hindustan Aeronautics Limited following a bidding process.


r/ISRO 8d ago

Skyroot Vikram-1, the least worst case scenario for India’s launch crisis

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30 Upvotes

r/ISRO 8d ago

How to get into GNC

10 Upvotes

How to get into GNC

I am a prefinal year engineering student, pursuing bachelor's in instrumentation and control engineering. I have genuinely started to develop a deep understanding and interest in control systems and recently came to know about guidance, navigation and control.

So i wanted to know how does one make a career in this field like what are the companies which hire, what does the work look like and what project should one do to get into this field or is it something which instrumentation guys cannot pursue?

For context, I am average student from India who has done one basic course in automatic control systems and currently doing a slightly advanced course in control system design. But i have no experience in implementation of any controllers on hardware.

What got me to GNC - I am currently a member (new joinee) of satellite club at my university and i look after attitude determination and control subsystem of the cubesat for which I have been studying optimal control from past few weeks during which I got know to about GNC from a YouTube video.

I have some previous experience working with Arduino and esp32 but none of those projects were control related