{"id":23591,"date":"2026-02-11T19:33:54","date_gmt":"2026-02-11T11:33:54","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/proton-m-launches-elektro-l-no-5-on-its-final-mission-with-blok-dm-upper-stage\/"},"modified":"2026-02-11T19:33:54","modified_gmt":"2026-02-11T11:33:54","slug":"proton-m-launches-elektro-l-no-5-on-its-final-mission-with-blok-dm-upper-stage","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/proton-m-launches-elektro-l-no-5-on-its-final-mission-with-blok-dm-upper-stage\/","title":{"rendered":"Proton-M launches Elektro-L No.5 on its final mission with Blok-DM upper stage"},"content":{"rendered":"<p>Russia\u2019s Proton rocket made its first flight in almost three years on Thursday, carrying the Elektro-L No.5 weather satellite into orbit. The launch, expected to be the last time Proton flies with a Blok-DM upper stage, took place at 08:52 UTC from Site 81\/24 at the Baikonur Cosmodrome in Kazakhstan.<\/p>\n<\/p>\n<p>Proton, once a workhorse of the Soviet and later Russian space programs, is now very much in the twilight years of its career. First flown in 1965, the rocket has made over 400 launches in various configurations; however, since 2020, it has carried out only a handful of missions as Russia transitions to its replacement, the Angara. Prior to the Elektro-L No.5 launch, Proton\u2019s last flight came in March 2023, when it deployed an Olymp-K spy satellite for the Russian security services. This is the longest gap between launches in Proton\u2019s history, with 2024 marking the first calendar year since its introduction without a single Proton launch.<\/p>\n<p>Thursday\u2019s launch is currently expected to be the last Proton mission with the Blok DM-03 upper stage, and by extension, the wider Blok-D family. Proton\u2019s remaining launches will use either the Briz-M or fly with no upper stage. Variants of the Blok DM-03 remain in production for use with other rockets such as Angara, but Thursday\u2019s launch marks the end of a relationship between a rocket and a series of upper stages that began in 1967 and enabled many of the Soviet Union\u2019s interplanetary missions and communications satellite launches.<\/p>\n<p>Elektro-L No.5 weather satellite and OChR secondary payload<\/p>\n<p>The primary payload for this launch was Elektro-L No.5, a geostationary weather satellite to be operated by Russia\u2019s federal space agency, Roscosmos. This is the fifth Elektro-L satellite to be launched, following earlier members of the series deployed in 2011, 2015, 2019, and 2023. The first two satellites were launched by Zenit rockets, and subsequent launches used Proton rockets.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" aria-describedby=\"caption-attachment-111953\" class=\"wp-image-111953 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L-4.jpg\" alt=\"\" width=\"678\" height=\"680\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L-4.jpg 678w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L-4-350x350.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L-4-349x350.jpg 349w\" sizes=\"(max-width: 678px) 100vw, 678px\"><\/p>\n<p id=\"caption-attachment-111953\" class=\"wp-caption-text\">A previous Elektro-L satellite, Elektro-L No.4, undergoing launch preparations. (Credit: Roscosmos)<\/p>\n<p>Elektro-L satellites form the geostationary component of Russia\u2019s fleet of weather satellites, complementing the low-Earth orbit (LEO) Meteor series. Operating in geostationary orbit allows each satellite to maintain a constant view of the same part of the Earth\u2019s surface. Constructed by NPO Lavochkin, the satellite has a mass of just over 2,000 kg and is expected to operate for at least 10 years.<\/p>\n<p>The satellite\u2019s primary instrument \u2014 Multispectral Scanner \u2013 Geostationary (MSU-GS) \u2014 images the full disk of the Earth in ten different spectral bands: three visible-light and seven infrared. It has a resolution of up to one kilometer in the visible-light and shorter-wavelength infrared bands, dropping to four kilometers at longer infrared wavelengths. A secondary instrument package, Helio-Geophysical Instrument Complex on Elektro-L (GGAK-E), uses a suite of sensors to measure solar radiation and magnetic fields, helping to forecast space weather and its effects on the Earth.<\/p>\n<p>SpaceX launch tickets<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>Space Shuttle<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>SpaceX<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>The Elektro-L satellites also carry two communications payloads: the Onboard Data Sampling System (ODSS) transmits data between Moscow and remote monitoring stations in the far East, while a Geostationary Search and Rescue System (GEOSAR) package relays emergency signals as part of the international COSPAS-SARSAT network.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-111954\" class=\"wp-image-111954 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-18.jpeg\" alt=\"\" width=\"1280\" height=\"720\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-18.jpeg 1280w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-18-350x197.jpeg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-18-622x350.jpeg 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-18-768x432.jpeg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-18-1170x658.jpeg 1170w\" sizes=\"(max-width: 1280px) 100vw, 1280px\"><\/p>\n<p id=\"caption-attachment-111954\" class=\"wp-caption-text\">Proton-M\/DM-03 at the launch pad for the Elektro-L No.5 mission. (Credit: Roscosmos)<\/p>\n<p>A second satellite, OChR, launched alongside Elektro-L No.5 as a secondary payload. No details of this co-passenger have been announced, but its name appears to be an abbreviation of the Russian for \u201corbit spectrum,\u201d which suggests the satellite will be used as a placeholder to secure Russia\u2019s allocation of communications frequencies or a slot in geostationary orbit intended to be used by a delayed mission in danger of missing its deadline to use them.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>Elektro-L No.5 Updates<\/li>\n<li>Russian Launchers Section<\/li>\n<li>NSF Store<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>Proton-M and Blok-DM upper stage<\/p>\n<p>The Proton-M\/DM-03 rocket that launched Elektro-L No.5 was a four-stage vehicle, consisting of a three-stage Proton-M and a Blok DM-03 upper stage to carry the satellite to its final orbit. Proton-M was first flown in 2001 as an upgraded version of the earlier Proton-K, whose design dated back to the 1960s. Vladimir Chelomei designed the then two-stage UR-500 as an exceptionally large ballistic missile, as part of the Universalnaya Raketa (UR, or Universal Rocket) series developed by his design bureau.<\/p>\n<p>While the UR-500 was too large to be practical as a missile, it was adapted to carry four heavy scientific satellites, the Proton, into orbit between 1965 and 1966. Taking its name from these satellites, the Proton-K first flew in 1967, with modifications to its second stage and a new third stage added to optimize it for orbital missions. The majority of Protons have flown in four-stage configurations, with an upper stage enabling launches to higher or more complex orbits than the core vehicle could reach on its own. When flown without an upper stage, Proton has been used to carry some of the Soviet Union and Russia\u2019s heaviest payloads, including space stations and large space station modules.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-111990\" class=\"size-full wp-image-111990\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/IMG_20251110_153853_638.jpg\" alt=\"\" width=\"900\" height=\"720\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/IMG_20251110_153853_638.jpg 900w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/IMG_20251110_153853_638-350x280.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/IMG_20251110_153853_638-438x350.jpg 438w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/IMG_20251110_153853_638-768x614.jpg 768w\" sizes=\"(max-width: 900px) 100vw, 900px\"><\/p>\n<p id=\"caption-attachment-111990\" class=\"wp-caption-text\">Elektro-L No.5 is delivered to Baikonur ahead of its launch. (Credit: Roscosmos)<\/p>\n<p>Two families of upper stages have been used in conjunction with Proton: Blok-D and Briz-M. The Blok-D family uses kerosene and liquid oxygen as propellants, while the Briz-M uses storable hypergolic propellants, as Proton does. Briz-M was first flown in 1999 and has been used on the majority of Proton launches since the mid-2000s, while Blok-D made its debut on the first Proton-K launch in 1967, with Thursday\u2019s launch expected to be its last on Proton, in the form of the significantly-upgraded Blok DM-03.<\/p>\n<p>Blok-D was developed as the fifth stage of the Soviet Union\u2019s N1 moon rocket, and its earliest flights on Proton were in support of the lunar program: tests with the 7K-L1 spacecraft, a stripped-down Soyuz which would have carried cosmonauts on a flyby of the Moon. The Proton-K\/Blok-D combination was also used to launch Lunokhod rovers and sample-return missions to the Moon, as well as probes to Mars and Venus.<\/p>\n<p>In 1974, the introduction of the Blok-DM, a Blok-D upgraded and optimised for Earth orbit missions, gave Russia access to geostationary orbit (GEO) for the first time, with Proton beginning to deploy communications and military satellites to GEO over the following years. Shortly after the introduction of the Blok-DM, an upgraded Blok D-1 replaced the Blok-D for interplanetary work.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-111956\" class=\"wp-image-111956 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L5-Blok-DM.jpg\" alt=\"\" width=\"1568\" height=\"892\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L5-Blok-DM.jpg 1568w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L5-Blok-DM-350x199.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L5-Blok-DM-615x350.jpg 615w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L5-Blok-DM-768x437.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Elektro-L5-Blok-DM-1170x666.jpg 1170w\" sizes=\"(max-width: 1568px) 100vw, 1568px\"><\/p>\n<p id=\"caption-attachment-111956\" class=\"wp-caption-text\">Blok DM-03 during pre-launch processing for the Elektro-L No.5 mission. (Credit: Roscosmos)<\/p>\n<p>An upgraded Blok DM-2 was introduced in 1982 to enable Proton\u2019s deployment of Uragan satellites for the Soviet GLONASS navigation system, with the DM-2 eventually replacing the Blok-DM for geostationary missions. A corresponding Blok D-2 was used to launch the twin Fobos missions to Mars\u2019s moon Phobos in 1988, and Russia\u2019s ill-fated 1996 Mars mission. In the 1990s, a version of the Blok DM-2 was adapted to use synthetic kerosene as the Blok DM-2M, while the Blok DM-5 was optimised for LEO missions.<\/p>\n<p>Marketed by International Launch Services (ILS), Proton was at the forefront of Russia\u2019s efforts to compete for commercial satellite launches in the 1990s following the fall of the Soviet Union, with Blok-DM variants used before the introduction of the Briz-M. Confusingly, ILS adopted its own designation system for the Blok-DM, which is usually written without a hyphen. The designation Blok DM1 corresponded to the Blok DM-2; DM2 corresponded to the DM-5; and DM3 and DM4 were used for different configurations of the Blok DM-2M.<\/p>\n<p>Once Briz-M was in service, the Blok DM-2 continued to be used for a decreasing number of military launches with older satellites \u2013 in particular, Uragan and Uragan-M GLONASS satellites, which were carried in groups of three. The final Blok DM-2 launch took place in 2012 with a US-KMO missile detection satellite, Kosmos 2479.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-111989\" class=\"size-full wp-image-111989\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088.jpg\" alt=\"\" width=\"1280\" height=\"853\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088.jpg 1280w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088-350x233.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088-525x350.jpg 525w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088-768x512.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088-1170x780.jpg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088-585x390.jpg 585w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/5314296763902529088-263x175.jpg 263w\" sizes=\"(max-width: 1280px) 100vw, 1280px\"><\/p>\n<p id=\"caption-attachment-111989\" class=\"wp-caption-text\">Proton is integrated ahead of its launch of the fifth Elektro-L satellite. (Credit: Roscosmos)<\/p>\n<p>The Blok DM-03 was developed as a successor to the Blok DM-2 on Proton, but was also designed for use with other rockets \u2014 including Zenit and Angara. It suffered an inauspicious start to its career, with the first two Proton-M\/DM-03 launches failing to reach orbit, though in both cases this was due to mistakes during pre-launch preparations rather than faulty rockets. The maiden flight took place in December 2010, but technicians familiar with the fueling procedures for the smaller Blok DM-2 loaded an incorrect amount of propellant into the vehicle, rendering it too heavy to make orbit on the programmed flight profile.<\/p>\n<p>The second launch came in July 2013. Accelerometers in Proton\u2019s first stage had been installed incorrectly, causing the onboard computers to receive faulty data on the vehicle\u2019s speed and orientation. The rocket went out of control seconds after liftoff and crashed back to Earth a few miles from the launch pad. Since then, Proton-M has flown five consecutive successful missions with the Blok DM-03, with the Elektro-L No.5 mission marking the eighth flight of this configuration overall.<\/p>\n<p>With the end of Blok-DM\u2019s service on Proton, the stage will continue to fly atop the Angara rocket under the designations Persei and Orion, and may also feature on the future Soyuz-5 rocket, which is expected to make its maiden flight later this year.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-111957\" class=\"wp-image-111957 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-17.jpeg\" alt=\"\" width=\"1280\" height=\"720\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-17.jpeg 1280w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-17-350x197.jpeg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-17-622x350.jpeg 622w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-17-768x432.jpeg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-17-1170x658.jpeg 1170w\" sizes=\"(max-width: 1280px) 100vw, 1280px\"><\/p>\n<p id=\"caption-attachment-111957\" class=\"wp-caption-text\">Proton arriving at Site 81\/24. (Credit: Roscosmos)<\/p>\n<p>Proton\u2019s launch and mission timeline<\/p>\n<p>Thursday\u2019s launch took place from Site 81\/24 at the Baikonur Cosmodrome in Kazakhstan. Site 81 was the first Proton launch complex built at Baikonur, and originally consisted of two pads, although pad 81\/23 has not been used since 2005. A second two-pad complex was built at Site 200 in the 1970s, and, like Site 81, it has one pad operational while the other has been decommissioned. It is unclear how much longer Pad 24 will remain operational, as it was reported to be at the end of its operational life in 2019, but has continued to host launches since then.<\/p>\n<p>The launch began with the ignition of the six RD-276 engines powering Proton\u2019s first stage. These burned unsymmetrical dimethylhydrazine (UDMH), oxidized by dinitrogen tetroxide, the same propellant mix used on the first three stages of the rocket. The first stage burned for the first two minutes of flight, as the rocket lifted off and began its climb through the atmosphere.<\/p>\n<p>Shortly before the first stage burned out, the second stage ignited its four engines. Proton uses a \u201chot staging\u201d separation sequence, where the second stage ignites while the first stage is still firing. This ensures the rocket is always accelerating, simplifying the process of delivering propellant to the second stage engines. Once the second stage is up and burning, the spent first stage can be shut down and jettisoned.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-111958\" class=\"wp-image-111958 size-full\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27.jpeg\" alt=\"\" width=\"1280\" height=\"853\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27.jpeg 1280w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27-350x233.jpeg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27-525x350.jpeg 525w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27-768x512.jpeg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27-1170x780.jpeg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27-585x390.jpeg 585w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2026\/02\/Proton-M-Elektro-L5-27-263x175.jpeg 263w\" sizes=\"(max-width: 1280px) 100vw, 1280px\"><\/p>\n<p id=\"caption-attachment-111958\" class=\"wp-caption-text\">Proton\u2019s first stage engines, seen during rollout to the launch pad. (Credit: Roscosmos)<\/p>\n<p>Proton\u2019s second stage engines consist of three RD-0210s and an RD-0211 \u2014 the latter being an RD-0210 with additional equipment to provide pressurization to the propellant tanks. The second stage burn lasted a little under three and a half minutes, after which it handed over to the third stage and separated. Proton\u2019s payload fairing also separated a few seconds into the burn. The third stage\u2019s RD-0212 propulsion unit fired for about four minutes, with its main engine shutting down a few seconds before its vernier (steering) engines and separation from Blok DM-03.<\/p>\n<p>Proton-M placed the Blok DM-03 and Elektro-L No.5 onto a suborbital trajectory. It coasted for about six minutes before Blok DM-03\u2019s RD-58M engine ignited for the first of three burns. Lasting just over a minute, this burn established an initial parking orbit in which the rocket and payload remained for about an hour. At about T+73 minutes after launch, Blok-DM\u2019s second burn began, with the stage firing for eight minutes to reach geostationary transfer orbit. The mission entered an extended coast phase before a third burn at about T+06:25 hours. This lasted about four minutes, placing the satellite into geostationary orbit.<\/p>\n<p>Elektro-L No.5 separated from Blok DM-03 just under eight minutes after the end of the third burn, around the scheduled time of T+06:37:49 hours. OChR separated eight minutes later, marking the end of Blok DM-03\u2019s mission.<\/p>\n<p>The Elektro-L launch ends a span of almost three years since the last Proton launch, which took place on March 12, 2023, the longest gap between launches in Proton\u2019s career. It is currently uncertain when the rocket\u2019s next launch will take place, but several more missions are planned before its retirement.<\/p>\n<p><em>(Lead image: Proton lifts off from the Baikonur Cosmodrome on the Elektro-L No.5 mission. Credit: Roscosmos)<\/em><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Russia\u2019s Proton rocket made its first flight in almost three years on Thursday, carrying the Elektro-L No.5 weather satellite into orbit. The launch, expected to be the last time Proton flies with a Blok-DM upper stage, took place at 08:52 UTC from Site 81\/24 at the Baikonur Cosmodrome in Kazakhstan. Proton, once a workhorse of [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[7831,1601,7896,7897,7898,2110,7899,234,7900,7901,650],"class_list":["post-23591","post","type-post","status-publish","format-standard","hentry","category-news","tag-baikonur","tag-baikonur-cosmodrome","tag-blok-dm","tag-elektro-l","tag-elektro-l-no-5","tag-proton","tag-proton-m","tag-roscosmos","tag-russian","tag-site-81-24","tag-weather"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/23591"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=23591"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/23591\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=23591"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=23591"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=23591"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}