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		<title>Ajay Kumar: Created a new article</title>
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		<summary type="html">&lt;p&gt;Created a new article&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{Infobox spaceflight&lt;br /&gt;
| name                  = PSLV-C35&lt;br /&gt;
| names_list            = Scatsat-1 mission&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--image of the spacecraft/mission--&amp;gt;&lt;br /&gt;
| image                 = PSLV.svg&lt;br /&gt;
| image_caption         = Model of the [[PSLV]] rocket&lt;br /&gt;
| image_alt             = &amp;lt;!--image alt text--&amp;gt;&lt;br /&gt;
| image_size            = 70px&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Basic details--&amp;gt;&lt;br /&gt;
| mission_type          = Deployment of eight [[satellite]]s in two different [[orbit]]s.&lt;br /&gt;
| operator              =[[ISRO]]&lt;br /&gt;
| Harvard_designation   = &amp;lt;!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)--&amp;gt;&lt;br /&gt;
| COSPAR_ID             = &amp;lt;!--spacecraft launched since 1963 only (aka NSSDC ID; eg. 1998-067A)--&amp;gt;&lt;br /&gt;
| SATCAT                = &amp;lt;!--satellite catalogue number, omit leading zeroes (e.g. 25544)--&amp;gt;&lt;br /&gt;
| website               = [http://www.isro.gov.in/ ISRO website]&lt;br /&gt;
| mission_duration      = 8,133 seconds&lt;br /&gt;
| distance_travelled    = &amp;lt;!--How far the spacecraft travelled (if known)--&amp;gt;&lt;br /&gt;
| orbits_completed      = &amp;lt;!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit--&amp;gt;&lt;br /&gt;
| suborbital_range      = &amp;lt;!--downrange distance reached if spacecraft did not enter orbit--&amp;gt;&lt;br /&gt;
| suborbital_apogee     =&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Spacecraft properties--&amp;gt;&lt;br /&gt;
| spacecraft            = [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
| spacecraft_type       = [[Expendable launch vehicle]]&lt;br /&gt;
| spacecraft_bus        = &amp;lt;!--eg. A2100M, Star-2, etc--&amp;gt;&lt;br /&gt;
| manufacturer          =[[ISRO]]&lt;br /&gt;
| launch_mass           = {{convert|320000|kg|lbs}}&lt;br /&gt;
| BOL_mass              = &amp;lt;!--spacecraft mass in orbit at beginning of operational life, after LEOP phase--&amp;gt;&lt;br /&gt;
| landing_mass          = &amp;lt;!--Mass after landing (recovered spacecraft only)--&amp;gt;&lt;br /&gt;
| dry_mass              = &amp;lt;!--spacecraft mass in orbit without fuel--&amp;gt;&lt;br /&gt;
| payload_mass          = {{convert|671.25|kg|lbs}}&lt;br /&gt;
| dimensions            = {{convert|44.4|m|ft|0}}&amp;lt;br&amp;gt;(overall height)&lt;br /&gt;
| power                 = &amp;lt;!--end-of-life power, in watts--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Launch details--&amp;gt;&lt;br /&gt;
| launch_date           = {{start date|2016|09|26|03|42|00|7=UTC}} ([[Coordinated Universal Time|UTC]])&lt;br /&gt;
| launch_rocket         = [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
| launch_site           = [[Satish Dhawan Space Centre First Launch Pad|Sriharikota Launching Range]]&lt;br /&gt;
| launch_contractor     =[[ISRO]]&lt;br /&gt;
| deployment_from       = &amp;lt;!--place where deployed from--&amp;gt;&lt;br /&gt;
| deployment_date       = &amp;lt;!--date deployed--&amp;gt;&lt;br /&gt;
| entered_service       = &amp;lt;!--date on which the spacecraft entered service, if it did not do so immediately after launch--&amp;gt;&lt;br /&gt;
&amp;lt;!-- * - e.g. Proton-M/Briz-M not Proton-M, but Titan IV(401)A not Titan IV(401)A-Centaur--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--end of mission--&amp;gt;&lt;br /&gt;
| disposal_type         = Not known&lt;br /&gt;
| deactivated           = {{end date|2016|09|26}}&lt;br /&gt;
| destroyed             = &amp;lt;!--when craft was destroyed (if other than by re-entry)--&amp;gt;&lt;br /&gt;
| last_contact          = &amp;lt;!--when last signal received if not decommissioned--&amp;gt;&lt;br /&gt;
| recovery_by           = &amp;lt;!--recovered by--&amp;gt;&lt;br /&gt;
| recovery_date         = &amp;lt;!--recovery date--&amp;gt;&lt;br /&gt;
| decay_date            = &amp;lt;!--when craft re-entered the atmosphere, not needed if it landed--&amp;gt;&lt;br /&gt;
| landing_date          = &amp;lt;!--when the spacecraft made a controlled landing, not needed if it did not return intact--&amp;gt;&lt;br /&gt;
| landing_site          = &amp;lt;!--where the craft landed; site/runway or coordinates--&amp;gt;&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
    The following template should be used for ONE of the three above fields &amp;quot;end_of_mission&amp;quot;, &amp;quot;decay&amp;quot; or &amp;quot;landing&amp;quot; if the spacecraft is no longer operational.&lt;br /&gt;
    If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered.&lt;br /&gt;
    {{end date|YYYY|MM|DD|hh|mm|ss|TZ=Z}} (for Zulu/UTC) or {{end date|YYYY|MM|DD}} (if time unknown) &lt;br /&gt;
--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--orbit parameters--&amp;gt;&lt;br /&gt;
&amp;lt;!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values--&amp;gt;&lt;br /&gt;
| orbit_reference       = [[Polar orbit]] and&amp;lt;br&amp;gt;[[Sun-synchronous orbit]]&lt;br /&gt;
| orbit_regime          = &lt;br /&gt;
| orbit_longitude       = &amp;lt;!--geosynchronous satellites only--&amp;gt;&lt;br /&gt;
| orbit_slot            = &amp;lt;!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)--&amp;gt;&lt;br /&gt;
| orbit_semimajor       = &amp;lt;!--semimajor axis--&amp;gt;&lt;br /&gt;
| orbit_eccentricity    = &amp;lt;!--orbital eccentricity--&amp;gt;&lt;br /&gt;
| orbit_periapsis       = &amp;lt;!--periapsis altitude--&amp;gt; &lt;br /&gt;
| orbit_apoapsis        = &amp;lt;!--apoapsis altitude--&amp;gt; &lt;br /&gt;
| orbit_inclination     = &amp;lt;!--orbit inclination--&amp;gt; &lt;br /&gt;
| orbit_period          = &amp;lt;!--time taken to complete an orbit--&amp;gt;&lt;br /&gt;
| orbit_RAAN            = &amp;lt;!--right ascension of the ascending node--&amp;gt;&lt;br /&gt;
| orbit_arg_periapsis   = &amp;lt;!--argument of perigee/periapsis--&amp;gt;&lt;br /&gt;
| orbit_mean_anomaly    = &amp;lt;!--mean anomaly at epoch, only use in conjunction with an epoch value--&amp;gt;&lt;br /&gt;
| orbit_mean_motion     = &amp;lt;!--mean motion of the satellite, usually measured in orbits per day--&amp;gt;&lt;br /&gt;
| orbit_repeat          = &amp;lt;!--repeat interval/revisit time--&amp;gt;&lt;br /&gt;
| orbit_velocity        = &amp;lt;!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity--&amp;gt;&lt;br /&gt;
| orbit_epoch           = &amp;lt;!--the date at which the orbit parameters were correct--&amp;gt;&lt;br /&gt;
| orbit_rev_number      = &amp;lt;!--revolution number--&amp;gt;&lt;br /&gt;
| apsis                 = &amp;lt;!--planet specific apsis term (eg. gee/helion/selene/etc - defaults to generic &amp;quot;apsis&amp;quot;)--&amp;gt;&lt;br /&gt;
|interplanetary         = &amp;lt;!--Infobox spaceflight/IP can be called multiple times for missions with multiple targets or combined orbiter/lander missions, etc--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Cargo parameters--&amp;gt;&lt;br /&gt;
| payload_items         = India [[ScatSat-1]], [[PISat]] &amp;amp; [[Pratham (satellite)|Pratham]],&amp;lt;br&amp;gt;Algeria [[Alsat-1B]], [[Alsat-2B]] &amp;amp; [[Alsat-1N]],&amp;lt;br&amp;gt;Canada,&amp;lt;br&amp;gt;United States [[Pathfinder-1]]&lt;br /&gt;
| cargo_mass            = {{convert|671.25|kg|lbs}}&lt;br /&gt;
| cargo_mass_press      = &amp;lt;!--Mass of pressurised cargo--&amp;gt;&lt;br /&gt;
| cargo_mass_unpress    = &amp;lt;!--Mass of unpressurised cargo (e.g. Dragon Trunk)--&amp;gt;&lt;br /&gt;
| cargo_mass_fuel       = &amp;lt;!--Mass of fuel transferred from spacecraft&amp;#039;s tanks--&amp;gt;&lt;br /&gt;
| cargo_mass_gas        = &amp;lt;!--Mass of gasses transferred (e.g. oxygen)--&amp;gt;&lt;br /&gt;
| cargo_mass_water      = &amp;lt;!--Mass of water transferred--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Telescope parameters--&amp;gt;&lt;br /&gt;
| instrument_type       = &amp;lt;!--converts telescope fields to suit a camera or other similar instrument--&amp;gt;&lt;br /&gt;
| telescope_name        = &amp;lt;!--name, if different to the satellite--&amp;gt;&lt;br /&gt;
| telescope_type        = &amp;lt;!--type of telescope, mirror arrangement, etc--&amp;gt; &lt;br /&gt;
| telescope_diameter    = &amp;lt;!--diameter of telescope--&amp;gt;&lt;br /&gt;
| telescope_focal_length= &amp;lt;!--focal length of telescope--&amp;gt;&lt;br /&gt;
| telescope_area        = &amp;lt;!--collecting area--&amp;gt;&lt;br /&gt;
| telescope_wavelength  = &amp;lt;!--wavelengths at which the telescope operates--&amp;gt; &lt;br /&gt;
| telescope_resolution  = &amp;lt;!--resolution of telescope--&amp;gt;&lt;br /&gt;
| instruments           = &amp;lt;!--a list of instruments on the satellite--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--transponder parameters--&amp;gt;&lt;br /&gt;
| trans_band            = &amp;lt;!--Transponder frequency bands--&amp;gt;&lt;br /&gt;
| trans_frequency       = &amp;lt;!--specific frequencies--&amp;gt;&lt;br /&gt;
| trans_bandwidth       = &amp;lt;!--bandwidth--&amp;gt;&lt;br /&gt;
| trans_capacity        = &amp;lt;!--capacity of the transponders--&amp;gt;&lt;br /&gt;
| trans_coverage        = &amp;lt;!--area covered--&amp;gt;&lt;br /&gt;
| trans_TWTA            = &amp;lt;!--TWTA output power--&amp;gt;&lt;br /&gt;
| trans_EIRP            = &amp;lt;!--equivalent isotropic power--&amp;gt;&lt;br /&gt;
| trans_HPBW            = &amp;lt;!--half-power beam width--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--Only use where a spacecraft/mission is part of a clear programme of sequential missions. &lt;br /&gt;
If in doubt, leave it out--&amp;gt;&lt;br /&gt;
| programme             = &amp;#039;&amp;#039;&amp;#039;[[Polar Satellite Launch Vehicle#Launch history|Polar Satellite Launch Vehicle missions]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
| previous_mission      = &amp;#039;&amp;#039;&amp;#039;[[PSLV-C34]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
| next_mission          = &amp;#039;&amp;#039;&amp;#039;[[PSLV-C36]]&amp;#039;&amp;#039;&amp;#039;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--mission insignia or patch--&amp;gt;&lt;br /&gt;
| insignia              = &lt;br /&gt;
| insignia_caption      = &lt;br /&gt;
| insignia_alt          = &amp;lt;!--image alt text--&amp;gt;&lt;br /&gt;
| insignia_size         = &amp;lt;!--include px/em; defaults to 180px--&amp;gt;&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
&amp;#039;&amp;#039;&amp;#039;PSLV-C35&amp;#039;&amp;#039;&amp;#039; was the successful mission of the [[Polar Satellite Launch Vehicle]] program which set eight satellites in space. It was launched on 26 September 2016 by [[Indian Space Research Organisation]] (ISRO) from the [[Satish Dhawan Space Centre]] at [[Sriharikota]].&lt;br /&gt;
&lt;br /&gt;
==Launch==&lt;br /&gt;
PSLV-C35 was launched at 03:42 hours [[Coordinated Universal Time]] (09:12 hours [[Indian Standard Time]]) on 26 September 2016 from the [[Satish Dhawan Space Centre First Launch Pad|first launch pad of Satish Dhawan Space Centre]] at [[Sriharikota]] in the Indian [[States and territories of India|state]] of [[Andhra Pradesh]].&amp;lt;ref name=&amp;quot;PSLV-C35&amp;quot;&amp;gt;{{cite news|title=PSLV-C35|publisher=[[ISRO]] website|accessdate=26 September 2016|url=http://www.isro.gov.in/launcher/pslv-c35-scatsat-1}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;ISRO’s PSLV-C35 places SCATSAT-1 in orbit&amp;quot;&amp;gt;{{cite news|title=ISRO&amp;#039;s PSLV-C35 places SCATSAT-1 in orbit|work=[[The Times of India]]|accessdate=28 September 2016|url=http://timesofindia.indiatimes.com/india/Isros-PSLV-C35-places-SCATSAT-1-weather-satellite-in-orbit-mission-is-on/articleshow/54517632.cms}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Mission highlights==&lt;br /&gt;
PSLV-C35 was the 37th launch of the [[PSLV]] program. It was also the 102nd overall launch by [[Indian Space Research Organisation]]. PSLV-C35 was the first spaceflight by ISRO to place satellites in two different orbits with a single rocket. It carried and injected eight satellites built by India, [[Algeria]], Canada and United States.&amp;lt;ref name=&amp;quot;PSLV-C35&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C35 brochure&amp;quot;&amp;gt;{{cite news|title=PSLV-C35 brochure|publisher=[[ISRO]] website|accessdate=26 September 2016|url=http://www.isro.gov.in/sites/default/files/flipping_book/PSLV_C35_4/files/assets/common/downloads/PSLV%20C35%20Final.pdf}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;ISRO timeline&amp;quot;&amp;gt;{{cite news|title=ISRO timeline|publisher=[[ISRO]] website|accessdate=26 September 2016|url=http://www.isro.gov.in/about-isro/isros-timeline-1960s-to-today#102}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Mission parameters==&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Mass&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;Total liftoff weight:&amp;#039;&amp;#039; {{convert|320000|kg|lbs}}&lt;br /&gt;
** &amp;#039;&amp;#039;Payload weight:&amp;#039;&amp;#039; {{convert|671.25|kg|lbs}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Overall height&amp;#039;&amp;#039;&amp;#039;: {{convert|44.4|m|ft|1}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Propellant&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;First stage:&amp;#039;&amp;#039; [[Solid-fuel rocket|Solid]] [[Hydroxyl-terminated polybutadiene|HTPB based]] (138.2 + 6 x 8.9 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; [[Liquid fuel rocket|Liquid]] [[UH 25]] + {{N2O4}} (42 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; [[Solid-fuel rocket|Solid]] [[Hydroxyl-terminated polybutadiene|HTPB based]] (7.6 tonnes)&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; [[Liquid fuel rocket|Liquid]] [[Monomethylhydrazine|MMH]] + [[Mixed oxides of nitrogen|MON-3]] (2.5 tonnes)&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Engine&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;First stage:&amp;#039;&amp;#039; Core (PS 1) + 6 strap-on [[Propellant strap on motor|PSOM]]&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; [[Vikas (rocket engine)|Vikas]]&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; PS 3&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; PS 4&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;[[Thrust]]&amp;#039;&amp;#039;&amp;#039;:&lt;br /&gt;
** &amp;#039;&amp;#039;First stage:&amp;#039;&amp;#039; 4,762 + 645 x 6 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Second stage:&amp;#039;&amp;#039; 800 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Third stage:&amp;#039;&amp;#039; 246 [[Newton (unit)|kN]]&lt;br /&gt;
** &amp;#039;&amp;#039;Fourth stage:&amp;#039;&amp;#039; 7.3 x 2 [[Newton (unit)|kN]]&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Maximum altitude&amp;#039;&amp;#039;&amp;#039;: {{convert|739.314|km|mi|0}}&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Maximum velocity&amp;#039;&amp;#039;&amp;#039;:{{convert|7527.63|m/s|ft/s|0}} (recorded at time of PS-4 engine restart 2)&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Duration&amp;#039;&amp;#039;&amp;#039;: 8,133 seconds&lt;br /&gt;
&amp;lt;ref name=&amp;quot;PSLV-C35 brochure&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Payload==&lt;br /&gt;
PSLV-C35 carried and deployed eight satellites in two different [[orbit]]s in a single mission ([[Polar orbit|Polar]] and [[Sun-synchronous orbit]]). This was the first time India had placed satellites in two orbits in a single mission.&amp;lt;ref name=&amp;quot;PSLV puts 8 satellites in two different orbits&amp;quot;&amp;gt;{{cite news|title=PSLV puts 8 satellites in two different orbits|work=[[The Hindu]]|accessdate=28 September 2016|url=http://www.thehindu.com/sci-tech/science/isros-pslvc35-places-scatsat1-into-orbit-on-its-way-to-place-seven-others/article9149124.ece}}&amp;lt;/ref&amp;gt; The vehicle carried three satellites from India ([[ScatSat-1]], [[PISat]] &amp;amp; [[Pratham (satellite)|Pratham]]), three satellites from Algeria ([[Alsat-1B]], [[Alsat-2B|2B]] &amp;amp; [[Alsat-1N|1N]]), one each from Canada ([[NLS-19]]) and the United States ([[Pathfinder-1]]).&amp;lt;ref name=&amp;quot;PSLV-C35&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;PSLV-C35 brochure&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;ISRO PSLV-C35 launch&amp;quot;&amp;gt;{{cite news|title=ISRO PSLV-C35 launch|publisher=[[Firstpost]]|accessdate=28 September 2016|url=http://tech.firstpost.com/news-analysis/isro-pslv-c35-launch-these-are-the-8-satellites-on-board-337090.html}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable sortable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! Country !! Owner !! Name !! Nos !! Mass !! Type !! Objective&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;3&amp;quot; | {{Flagicon|India}} India || [[ISRO]] || [[ScatSat-1]] || 1 || 377&amp;amp;nbsp;kg || [[Miniaturized satellite]] || [[Weather satellite|Weather forecasting]], [[cyclone]] prediction and tracking.&lt;br /&gt;
|-&lt;br /&gt;
| [[Indian Institute of Technology Bombay|IIT Bombay]] || [[Pratham (satellite)|Pratham]] || 1 || 10&amp;amp;nbsp;kg || rowspan=&amp;quot;2&amp;quot; | [[Nanosatellite]] || [[Research satellites|Research satellite]].&lt;br /&gt;
|-&lt;br /&gt;
| [[PES University|PES Institute of Technology]] || [[PISat]] || 1 || 5.25&amp;amp;nbsp;kg || [[Remote sensing]].&amp;lt;ref name=&amp;quot;PSLV-C35 brochure&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;ISRO PSLV-C35 launch&amp;quot;/&amp;gt;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;3&amp;quot; | {{Flagicon|Algeria}} [[Algeria]] || rowspan=&amp;quot;3&amp;quot; | [[Agence Spatiale Algerienne]] || [[Alsat-1B]] || 1 || 103&amp;amp;nbsp;kg || rowspan=&amp;quot;2&amp;quot; | [[Earth observation satellite]] || Agricultural and disaster monitoring.&lt;br /&gt;
|-&lt;br /&gt;
| [[Alsat-2B]] || 1 || 117&amp;amp;nbsp;kg || Monitoring natural resources.&lt;br /&gt;
|-&lt;br /&gt;
| [[Alsat-1N]] || 1 || 7&amp;amp;nbsp;kg || rowspan=&amp;quot;2&amp;quot; | [[Nanosatellite]] || rowspan=&amp;quot;2&amp;quot; | [[Technology demonstration]] satellite.&amp;lt;ref name=&amp;quot;PSLV-C35 brochure&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;ISRO PSLV-C35 launch&amp;quot;/&amp;gt;&lt;br /&gt;
|-&lt;br /&gt;
| {{Flagicon|Canada}} [[Canada]] || [[University of Toronto Institute for Aerospace Studies|UTIAS]] || [[NLS-19]] || 1 || 8&amp;amp;nbsp;kg&lt;br /&gt;
|-&lt;br /&gt;
| {{Flagicon|United States}} [[United States|USA]] || [[Spaceflight Industries]] || [[Pathfinder-1]] || 1 || 44&amp;amp;nbsp;kg || [[Earth observation satellite|Earth observation]], [[Micro-satellites|micro-satellite]] || Earth imaging.&amp;lt;ref name=&amp;quot;PSLV-C35 brochure&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;ISRO PSLV-C35 launch&amp;quot;/&amp;gt;&lt;br /&gt;
|-&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
* [[Indian Space Research Organisation]]&lt;br /&gt;
* [[Polar Satellite Launch Vehicle]]&lt;br /&gt;
&lt;br /&gt;
{{Portal bar|India|Science|Space|Spaceflight}}&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
{{Reflist|colwidth=30em}}&lt;br /&gt;
{{PSLV}}&lt;br /&gt;
{{Indian space programme}}&lt;br /&gt;
{{Expendable launch systems}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Spacecraft launched by India in 2016]]&lt;br /&gt;
[[Category:Polar Satellite Launch Vehicle]]&lt;/div&gt;</summary>
		<author><name>Ajay Kumar</name></author>
	</entry>
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