Soyuz-2-1A

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Soyuz-2-1A

Part of R-7

Russian orbital launch vehicle. Updated version using a new digital flight control system (replacing the old analogue system, increasing payload by 300 kg.

AKA: 14A14. Status: Active. First Launch: 2004-11-08. Last Launch: 2018-07-09. Number: 30 .

More at: Soyuz-2-1A.

Country: Russia. Spacecraft: Aist, Bars, Bion-M, Proteus, Vostok, Yantar-4K1, Progress M, SPOT-5A-5B, Cubesat, Metop, Meridian, ISS Japanese Experiment Module. Launch Sites: Baikonur LC31, Plesetsk LC43/4, Plesetsk LC43/3.

2004 November 8 - . 18:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Soyuz 2 flight test. - . Nation: Russia. Agency: KVR.
First flight test of a modernized version of the Soyuz ST equipped with a digital control system. Suborbital launch; carried an obsolete Zenit-8 reconnaisance satellite as a mass model and impacted in the Pacific Ocean. Launch delayed from October 15 and 29, November 6.

2006 October 19 - . 16:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Metop-A - . Mass: 4,093 kg (9,023 lb). Nation: Europe. Agency: RKA. Class: Earth. Type: Weather satellite. Spacecraft Bus: SPOT-5A-5B. Spacecraft: Metop. USAF Sat Cat: 29499 . COSPAR: 2006-044A. Apogee: 817 km (507 mi). Perigee: 817 km (507 mi). Inclination: 98.70 deg. Period: 101.00 min.
European polar weather satellite equipped with high-resolution visible and infrared cameras, a microwave sounder, ozone monitors, a GPS atmospheric sounding device, a wind scatterometer, and a search and rescue package. First launch of the Soyuz 2 version of the venerable Soyuz launch vehicle. The main change in this first version of the new booster was a digital control system. Problems with this system delayed the launch repeatedly.

2006 December 24 - . 08:34 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Meridian 1 - . Mass: 2,000 kg (4,400 lb). Nation: Russia. Agency: VKS. Manufacturer: Reshetnev bureau. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. USAF Sat Cat: 29668 . COSPAR: 2006-061A. Apogee: 39,093 km (24,291 mi). Perigee: 1,264 km (785 mi). Inclination: 63.40 deg. Period: 717.80 min.
Launch rescheduled twice due to Soyuz 2 software problems. The Meridian satellite was designed to provide communication between vessels and airplanes involved in ice surveillance in the North Sea area, and coastal stations on the ground, as well as to expand a network of satellite communications in the northern regions of Siberia and the Russian Far East.

2009 May 21 - . 21:53 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Meridian 2 - . Mass: 2,000 kg (4,400 lb). Nation: Russia. Agency: KVR. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. USAF Sat Cat: 35008 . COSPAR: 2009-029A. Apogee: 36,423 km (22,632 mi). Perigee: 328 km (203 mi). Inclination: 62.90 deg. Period: 646.00 min. Secon Meridian communications satellite. Third stage cut off early. Fregat upper stage ran out of fuel during second burn, leaving satellite in useless orbit..

2010 October 19 - . 17:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Globalstar M079 - . Payload: Globalstar-2 M079. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37188 . COSPAR: 2010-054A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min. First six or 48 new-generation Globalstar-2 satellites that will replace the 44 operational Globalstar satellites already aloft..

Globalstar M074 - . Payload: Globalstar-2 M074. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37189 . COSPAR: 2010-054B. Apogee: 1,415 km (879 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.

Globalstar M076 - . Payload: Globalstar-2 M076. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37190 . COSPAR: 2010-054C. Apogee: 1,415 km (879 mi). Perigee: 1,412 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.

Globalstar M077 - . Payload: Globalstar-2 M077. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37191 . COSPAR: 2010-054D. Apogee: 993 km (617 mi). Perigee: 951 km (590 mi). Inclination: 52.00 deg. Period: 104.50 min.

Globalstar M075 - . Payload: Globalstar-2 M075. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37192 . COSPAR: 2010-054E. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.

Globalstar M073 - . Payload: Globalstar-2 M073. Mass: 700 kg (1,540 lb). Nation: USA. Agency: RKA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37193 . COSPAR: 2010-054F. Apogee: 1,004 km (623 mi). Perigee: 955 km (593 mi). Inclination: 52.00 deg. Period: 104.70 min.

2010 November 2 - . 00:59 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Meridian 3 - . Mass: 2,000 kg (4,400 lb). Nation: Russia. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. USAF Sat Cat: 37212 . COSPAR: 2010-058A. Apogee: 39,395 km (24,478 mi). Perigee: 957 km (594 mi). Inclination: 62.80 deg. Period: 717.70 min. Third military communications satellite in this series..

2011 May 4 - . 17:41 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Meridian 4 - . Payload: Meridian No. 14L. Mass: 2,000 kg (4,400 lb). Nation: Russia. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. USAF Sat Cat: 37398 . COSPAR: 2011-018A. Apogee: 39,739 km (24,692 mi). Perigee: 968 km (601 mi). Inclination: 62.80 deg. Period: 724.90 min. Communications for the Russian Defense Ministry, and replacing the older Molniya satellites..

2011 July 13 - . 02:27 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Globalstar M08 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37739 . COSPAR: 2011-033A. Apogee: 932 km (579 mi). Perigee: 920 km (570 mi). Inclination: 52.00 deg. Period: 103.50 min.

Globalstar M08 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37740 . COSPAR: 2011-033B. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.

Globalstar M09 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37741 . COSPAR: 2011-033C. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.10 min.

Globalstar M08 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37742 . COSPAR: 2011-033D. Apogee: 931 km (578 mi). Perigee: 916 km (569 mi). Inclination: 52.00 deg. Period: 103.50 min.

Globalstar M08 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37743 . COSPAR: 2011-033E. Apogee: 1,178 km (731 mi). Perigee: 1,103 km (685 mi). Inclination: 52.00 deg. Period: 108.10 min. Second batch of six second-generation Globalstar low-orbit communications satellites launched on a single booster..

Globalstar M08 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 37744 . COSPAR: 2011-033F. Apogee: 932 km (579 mi). Perigee: 916 km (569 mi). Inclination: 52.00 deg. Period: 103.50 min.

2011 December 28 - . 17:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Globalstar M084 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 38040 . COSPAR: 2011-080A. Apogee: 926 km (575 mi). Perigee: 921 km (572 mi). Inclination: 52.00 deg. Period: 103.50 min. Replenishment of Globalstar MEO constellation..

Globalstar M080 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 38041 . COSPAR: 2011-080B. Apogee: 926 km (575 mi). Perigee: 920 km (570 mi). Inclination: 52.00 deg. Period: 103.50 min.

Globalstar M082 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 38042 . COSPAR: 2011-080C. Apogee: 926 km (575 mi). Perigee: 918 km (570 mi). Inclination: 52.00 deg. Period: 103.50 min.

Globalstar M092 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 38043 . COSPAR: 2011-080D. Apogee: 926 km (575 mi). Perigee: 916 km (569 mi). Inclination: 52.00 deg. Period: 103.40 min.

Globalstar M090 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 38044 . COSPAR: 2011-080E. Apogee: 926 km (575 mi). Perigee: 917 km (569 mi). Inclination: 52.00 deg. Period: 103.40 min.

Globalstar M086 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Proteus. USAF Sat Cat: 38045 . COSPAR: 2011-080F. Apogee: 926 km (575 mi). Perigee: 919 km (571 mi). Inclination: 52.00 deg. Period: 103.50 min.

2012 September 17 - . 16:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

METOP-B - . Mass: 4,244 kg (9,356 lb). Nation: Europe. Class: Earth. Type: Weather satellite. Spacecraft: SPOT-5A-5B. USAF Sat Cat: 38771 . COSPAR: 2012-049A. Apogee: 811 km (503 mi). Perigee: 806 km (500 mi). Inclination: 98.70 deg. Period: 101.00 min. European weather satellite agency EUMETSAT's second METOP satellite..

2012 November 14 - . 11:42 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Meridian No. 16 - . Mass: 2,000 kg (4,400 lb). Nation: Russia. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. USAF Sat Cat: 38995 . COSPAR: 2012-063A. Apogee: 39,732 km (24,688 mi). Perigee: 986 km (612 mi). Inclination: 62.80 deg. Period: 725.20 min. Sixth Meridian military communications satellite for the Russian Defense Ministry..

2013 February 6 - . 16:04 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. Launch Pad: LC31/6. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Globalstar M097 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 39072 . COSPAR: 2013-005A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.08 min.

Globalstar M093 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 39073 . COSPAR: 2013-005B. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 51.98 deg. Period: 114.08 min.

Globalstar M094 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 39074 . COSPAR: 2013-005C. Apogee: 927 km (576 mi). Perigee: 916 km (569 mi). Inclination: 52.01 deg. Period: 103.44 min.

Globalstar M096 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 39075 . COSPAR: 2013-005D. Apogee: 1,415 km (879 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.08 min.

Globalstar M078 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 39076 . COSPAR: 2013-005E. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 51.99 deg. Period: 114.08 min.

Globalstar M095 - . Mass: 700 kg (1,540 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Proteus. USAF Sat Cat: 39077 . COSPAR: 2013-005F. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 51.98 deg. Period: 114.08 min. Six satellites in one launch; replenishment of Globalstar MEO mobile-phone communications satellite constellation..

2013 April 19 - . 10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. Launch Pad: LC31/6. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Bion-M No. 1 - . Mass: 6,266 kg (13,814 lb). Nation: Russia. Class: Biology. Type: Biology satellite. Spacecraft: Bion-M. Decay Date: 2013-05-19 . USAF Sat Cat: 39130 . COSPAR: 2013-015A. Apogee: 579 km (359 mi). Perigee: 471 km (292 mi). Inclination: 64.88 deg. Period: 95.14 min.
The biosat combined a Vostok spherical pressurized reentry capusle and a Yantar service module. The capsule carried mice, gerbils, geckos, and snails; microorganisms in FRAGMENTER and BIOKONT-B containers; fish and algae in an OMEGAHAB aquarium; plants in FITO plant containers; and some microgravity materials experiments. Landed 82 km north of Orenburg at 03:12 GMT on 19 May. The gerbils had perished due to equipment failure; all of the geckos and half of the mice were alive

OSSI-1 - . Mass: 1.00 kg (2.20 lb). Nation: Korea South. Spacecraft: Cubesat. Decay Date: 2013-07-08 . USAF Sat Cat: 39131 . COSPAR: 2013-015B. Apogee: 348 km (216 mi). Perigee: 218 km (135 mi). Inclination: 64.86 deg. Period: 90.17 min. Cubesat developed by a Korean artist..

Dove-2 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 39132 . COSPAR: 2013-015C. Apogee: 575 km (357 mi). Perigee: 564 km (350 mi). Inclination: 64.87 deg. Period: 96.06 min. 3U cubesat, a demonstration satellite for Cosmogia, designed to return on-board system health data and validate the design for future Dove satellites, which will carry remote sensing payloads..

BEESAT-3 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Spacecraft: Cubesat. USAF Sat Cat: 39134 . COSPAR: 2013-015E. Apogee: 574 km (356 mi). Perigee: 558 km (346 mi). Inclination: 64.88 deg. Period: 95.97 min. 1U cubesat from the Technical University of Berlin. Reaction wheel technology qualification. Successful..

Aist 2 - . Mass: 39 kg (85 lb). Nation: Russia. Spacecraft: Aist. USAF Sat Cat: 39133 . COSPAR: 2013-015D. Apogee: 575 km (357 mi). Perigee: 564 km (350 mi). Inclination: 64.88 deg. Period: 96.05 min. Small satellite released from the side of Bion-M's service module, developed by TsSKB-Progress and the Samara Aerospace University; carried a magnetometer, acclerometers and a micrometeor experiment..

SOMP - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Spacecraft: Cubesat. USAF Sat Cat: 39135 . COSPAR: 2013-015F. Apogee: 574 km (356 mi). Perigee: 558 km (346 mi). Inclination: 64.88 deg. Period: 95.98 min. Student Oxygen Measurement 1U cubesat from Technical University of Dresden. Mission: Education, testing software defined radio, measuring atomic oxygen concentration, demonstrating TFSC ..

BEESAT-2 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Spacecraft: Cubesat. USAF Sat Cat: 39136 . COSPAR: 2013-015G. Apogee: 574 km (356 mi). Perigee: 558 km (346 mi). Inclination: 64.88 deg. Period: 95.98 min. 1U cubesat from the Technical University of Berlin. Mission: Reaction wheel technology qualification. Successful..

2014 May 6 - . 13:49 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Cosmos 2495 - . Payload: Kobalt-M. Mass: 6,700 kg (14,700 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Yantar. Spacecraft: Yantar-4K1. Decay Date: 2014-09-03 . USAF Sat Cat: 39732 . COSPAR: 2014-025A. Apogee: 253 km (157 mi). Perigee: 203 km (126 mi). Inclination: 81.40 deg. Period: 89.06 min. Kobalt-M spy satellite, serial number 564. Ninth launch of an 11F695M Kobalt-M film-return satellite and the first to use the Soyuz-2-1A rocket instead of the older Soyuz-U. By May 17 the satellite was in a 207 x 248 km x 81.4 deg orbit..

2014 July 18 - . 20:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Foton M4 - . Mass: 6,840 kg (15,070 lb). Nation: Russia. Agency: FKA. Class: Materials. Type: Materials science satellite. Spacecraft: Vostok. Decay Date: 2014-09-01 . USAF Sat Cat: 40095 . COSPAR: 2014-041A. Apogee: 530 km (320 mi). Perigee: 248 km (154 mi). Inclination: 64.88 deg. Period: 92.34 min.
Foton-M, using the Vostok reentry capsule, but a new extended length service module. Microgravity and life sciences experiments were on board, including geckos and tardigrades. The return capsule included samples exposed on the exterior for reentry studies. On July 24 it was revealed that the satellite was not responding to ground commands, although it continued to send back telemetry. Control was later reported to have been regained, but a scheduled orbit raise burn was cancelled, and on August 12 the orbit was still 250 x 542 km. Landed in the Orenburg district on September 1 at 09:18 GMT. The geckos carried as part of the payload were found to have died.

2014 October 29 - . 07:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1a.

Progress M-25M - . Payload: Progress M s/n 424 / ISS-57P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 179.00 days. Decay Date: 2015-04-26 . USAF Sat Cat: 40292 . COSPAR: 2014-067A. Apogee: 403 km (250 mi). Perigee: 396 km (246 mi). Inclination: 51.64 deg. Period: 92.56 min. Docked with the ISS Pirs module at 13:08 GMT 29 October. Undocked from the Pirs module at 06:41 GMT on April 25 and was deorbited on April 26, with debris falling in the South Pacific at 13:00 GMT..

2014 October 30 - . 01:43 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Meridian No. 17L - . Mass: 2,000 kg (4,400 lb). Nation: Russia. Class: Communications. Type: Communications satellite. Spacecraft Bus: Glonass. Spacecraft: Meridian. USAF Sat Cat: 40296 . COSPAR: 2014-069A. Apogee: 39,296 km (24,417 mi). Perigee: 1,056 km (656 mi). Inclination: 62.83 deg. Period: 717.73 min. Seventh in the series of communications satellites for the Russian Ministry of Defense in 12-hour Molniya orbits..

2015 February 27 - . 11:01 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Cosmos 2503 - . Payload: COSMOS 2503. Mass: 4,000 kg (8,800 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Yantar. Spacecraft: Bars. USAF Sat Cat: 40420 . COSPAR: 2015-009A. Apogee: 577 km (358 mi). Perigee: 566 km (351 mi). Inclination: 97.67 deg. Period: 96.09 min. Believed to be a new-generation electro-optical reconnaisance satellite based on a heavily modified Yantar bus. Sun synchronous orbit; 0245 GMT local time of the descending node..

2015 April 28 - . 07:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1a. FAILURE: The third stage did not shut down correctly and damaged the spacecraft during separation.. Failed Stage: 3.

Progress M-27M - . Payload: Progress M s/n 425 / ISS-59P. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress M. Duration: 10.00 days. Decay Date: 2015-05-08 . USAF Sat Cat: 40619 . COSPAR: 2015-024A. Apogee: 258 km (160 mi). Perigee: 186 km (115 mi). Inclination: 51.60 deg. Limited telemetry was obtained from the Progress, but Russian mission control was unable to control the damaged, spinning spacecraft. The Progress reentered over the South Pacific off the southwest coast of Chile at 02:20 GMT on May 8..

2015 June 5 - . 15:23 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Cosmos 2505 - . Mass: 6,700 kg (14,700 lb). Nation: Russia. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Yantar. Spacecraft: Yantar-4K1. Decay Date: 2015-09-18 . USAF Sat Cat: 40667 . COSPAR: 2015-027A. Apogee: 285 km (177 mi). Perigee: 177 km (109 mi). Inclination: 81.40 deg.
Kobal't-M spy satellite s/n 565, maneuvered on 8 and 13 June from an initial orbit of 177 km x 285 km x 81.4 deg to 203 km x 264 km. Current version of the Yantar satellite which returns its main section, with film and camera, to Earth at the end of its flight. It also carried two small ejectable film canisters which can return some data to Earth during the mission.

2015 December 21 - . 08:44 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Progress MS-01 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. Decay Date: 2016-07-03 . USAF Sat Cat: 41177 . COSPAR: 2015-080A. Apogee: 279 km (173 mi). Perigee: 270 km (160 mi). Inclination: 51.60 deg.
First Progress-MS cargo ship. Progress-MS was similar to previous Progress ships but with improved onboard systems. It docked with the Pirs module at 1027 UTC Dec 23. Progress MS-01 undocked from the Pirs module at 0536 UTC on Jul 1, backed off to 180m, and redocked at 0605 UTC under TORU remote control. During redocking there was an incorrect thruster firing that made the vehicle swing visibly from side to side. The problem was reportedly under investigation but did not affect Progress MS-01's final undocking, which happened at 0348 UTC Jul 3. Progress MS-01 was deorbited and destroyed over the South Pacifc at 0750 UTC Jul 3.

2016 March 24 - . 09:42 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Cosmos 2515 - . Payload: Bars-M No. 2. Nation: Russia. Class: Surveillance. Type: Cartographic satellite. Spacecraft Bus: Yantar. Spacecraft: Bars. USAF Sat Cat: 41394 . COSPAR: 2016-020A. Apogee: 540 km (330 mi). Perigee: 332 km (206 mi). Inclination: 97.60 deg. Bars-M cartography satellite; joined the No. 1 satellite (Kosmos-2503) launched in 2015. 1325LT SSO..

2016 March 31 - . 16:23 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Progress MS-02 - . Nation: Russia. Agency: RKA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Progress MS. Decay Date: 2016-10-14 . USAF Sat Cat: 41436 . COSPAR: 2016-022A. Apogee: 267 km (165 mi). Perigee: 261 km (162 mi). Inclination: 51.60 deg. Docked with Zvezda on Apr 2 at 1758 UTC..

2016 April 28 - . 02:01 GMT - . Launch Site: Vostochniy. Launch Complex: Vostochniy PU1S. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Lomonosov - . Payload: MVL 300. Nation: Russia. Class: Astronomy. Type: Astronomy satellite. USAF Sat Cat: 41464 . COSPAR: 2016-026A. Apogee: 486 km (301 mi). Perigee: 471 km (292 mi). Inclination: 97.30 deg.
Lomonosov (Mikhailo-Lomonosov-300) science satellite was orbited from the new Vostochniy spaceport. The old GIK-2 (2nd State Test Cosmodrome) at Svobodniy was shut down in 2007; its reopening as Vostochniy marks a planned shift away from the Kazakhstan launch site of Baikonur. Lomonosov's main experiment, TUS, was an ultraviolet camera to observe the flashes from cosmic rays hitting the Earth's upper atmosphere. 2314LT SSO.

AIST-2D - . Nation: Russia. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41465 . COSPAR: 2016-026B. Apogee: 485 km (301 mi). Perigee: 471 km (292 mi). Inclination: 97.30 deg. Samara State Aerospace University's AIST-2D imaging satellite;, the student-built Samsat-218/D failed to transmit properly..

Kontakt-NS - . Payload: SAMSAT 218D. Nation: Russia. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41466 . COSPAR: 2016-026C. Apogee: 485 km (301 mi). Perigee: 471 km (292 mi). Inclination: 97.30 deg. Samara State Aerospace University Kontakt-Nanosputnik (Samsat-218/D) cubesat. 2314LT SSO.

2017 June 14 - . 09:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Progress MS-06 - . Payload: Progress 7K-TGM No. 436. Nation: Russia. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Progress MS. USAF Sat Cat: 42756 . COSPAR: 2017-033A. Apogee: 406 km (252 mi). Perigee: 403 km (250 mi). Inclination: 51.64 deg. Period: 92.65 min. See Progress-MS 06. ..

2017 June 14 - . 09:19 GMT - . Launch Platform: ISS. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Tanyusha YuZGU No. 1 - . Payload: Radioskaf RS-6S; TANYUSHA 1. Nation: Russia. USAF Sat Cat: 42911 . COSPAR: 1998-067NA. Apogee: 341 km (211 mi). Perigee: 337 km (209 mi). Inclination: 51.63 deg. Period: 91.31 min. See Tanyusha-YuZGU 1 (Radioskaf RS-6) ↑. ..

Tanyusha YuZGU No. 2 - . Payload: Radioskaf RS-7S; TANYUSHA 2. Nation: Russia. USAF Sat Cat: 42912 . COSPAR: 1998-067NB. Apogee: 346 km (214 mi). Perigee: 341 km (211 mi). Inclination: 51.64 deg. Period: 91.41 min. See Tanyusha-YuZGU 2 (Radioskaf RS-7) ↑. ..

TS530-Zerkalo - . Payload: Sfera-53; SFERA 2. Nation: Russia. USAF Sat Cat: 42913 . COSPAR: 1998-067NC. Apogee: 153 km (95 mi). Perigee: 146 km (90 mi). Inclination: 51.61 deg. Period: 87.48 min. See Sfera-53 2 ↑. ..

TNS-0-2 Nanosputnik - . Payload: TEKh-42-2; TNS 0-2. Nation: Russia. USAF Sat Cat: 42914 . COSPAR: 1998-067ND. Apogee: 351 km (218 mi). Perigee: 347 km (215 mi). Inclination: 51.63 deg. Period: 91.52 min. See TNS 0-2 ↑. ..

2017 July 14 - . 06:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Kanopus-V-IK No. 2 - . Nation: Russia. USAF Sat Cat: 42825 . COSPAR: 2017-042A. Apogee: 510 km (310 mi). Perigee: 507 km (315 mi). Inclination: 97.45 deg. Period: 94.79 min. See Kanopus-V-IK 1. ..

NORSAT-1 - . Nation: TBD. USAF Sat Cat: 42826 . COSPAR: 2017-042B. Apogee: 606 km (376 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.59 min. See NORSAT 1. ..

Flock 2k-3 - . Payload: Dove 0F21; FLOCK 2K 03. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42850 . COSPAR: 2017-042AB. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 3 (Dove 0F21). ..

Flock 2k-43 - . Payload: Dove 1056; FLOCK 2K 43. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42874 . COSPAR: 2017-042BB. Apogee: 468 km (290 mi). Perigee: 451 km (280 mi). Inclination: 96.96 deg. Period: 93.79 min. See Flock-2k 43 (Dove 1056). ..

Flock 2k-4 - . Payload: Dove 0F24; FLOCK 2K 04. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42851 . COSPAR: 2017-042AC. Apogee: 457 km (283 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.58 min. See Flock-2k 4 (Dove 0F24). ..

Iskra-MAI-85 - . Nation: TBD. USAF Sat Cat: 42827 . COSPAR: 2017-042C. Apogee: 606 km (376 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.58 min. See Iskra-MAI-85. ..

Flock 2k-41 - . Payload: Dove 1054; FLOCK 2K 41. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42875 . COSPAR: 2017-042BC. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 41 (Dove 1054). ..

Flock 2k-36 - . Payload: Dove 104F; FLOCK 2K 36. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42876 . COSPAR: 2017-042BD. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 36 (Dove 104F). ..

NORSAT-2 - . Nation: TBD. USAF Sat Cat: 42828 . COSPAR: 2017-042D. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See NORSAT 2. ..

Flock 2k-1 - . Payload: Dove 0F1A; FLOCK 2K 01. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42852 . COSPAR: 2017-042AD. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 1 (Dove 0F1A). ..

Technosat - . Nation: Germany. USAF Sat Cat: 42829 . COSPAR: 2017-042E. Apogee: 606 km (376 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.58 min. See TechnoSat (Tubsat 12). ..

Flock 2k-35 - . Payload: Dove 104E; FLOCK 2K 35. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42877 . COSPAR: 2017-042BE. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 35 (Dove 104E). ..

Flock 2k-2 - . Payload: Dove 0F1E; FLOCK 2K 02. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42853 . COSPAR: 2017-042AE. Apogee: 465 km (288 mi). Perigee: 450 km (270 mi). Inclination: 96.96 deg. Period: 93.75 min. See Flock-2k 2 (Dove 0F1E). ..

Mayak - . Nation: TBD. USAF Sat Cat: 42830 . COSPAR: 2017-042F. Apogee: 604 km (375 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.54 min. See Mayak. ..

Flock 2k-47 - . Payload: Dove 1043; FLOCK 2K 47. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42854 . COSPAR: 2017-042AF. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 47 (Dove 1043). ..

Flock 2k-34 - . Payload: Dove 104D; FLOCK 2K 34. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42878 . COSPAR: 2017-042BF. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 34 (Dove 104D). ..

Flock 2k-48 - . Payload: Dove 101C; FLOCK 2K 48. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42855 . COSPAR: 2017-042AG. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 48 (Dove 101C). ..

FLP - . Payload: Flying Laptop. Nation: Germany. USAF Sat Cat: 42831 . COSPAR: 2017-042G. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.58 min. See Flying Laptop. ..

Flock 2k-33 - . Payload: Dove 104C; FLOCK 2K 33. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42879 . COSPAR: 2017-042BG. Apogee: 454 km (282 mi). Perigee: 439 km (272 mi). Inclination: 96.96 deg. Period: 93.51 min. See Flock-2k 33 (Dove 104C). ..

Ekvador-UTE-YuZGU - . Payload: UTE-UESOR. Nation: TBD. USAF Sat Cat: 42832 . COSPAR: 2017-042H. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See UTE-UESOR (Ecuador-UTE-YuZGU). ..

Flock 2k-28 - . Payload: Dove 1047; FLOCK 2K 28. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42880 . COSPAR: 2017-042BH. Apogee: 468 km (290 mi). Perigee: 452 km (280 mi). Inclination: 96.96 deg. Period: 93.79 min. See Flock-2k 28 (Dove 1047). ..

Flock 2k-45 - . Payload: Dove 100D; FLOCK 2K 45. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42856 . COSPAR: 2017-042AH. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 45 (Dove 100D). ..

Flock 2k-24 - . Payload: Dove 0F4F; FLOCK 2K 24. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42857 . COSPAR: 2017-042AJ. Apogee: 457 km (283 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 24 (Dove 0F4F). ..

Lemur-2-ArtFisher - . Payload: Lemur-2-43; LEMUR 2 ARTFISCHER. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42881 . COSPAR: 2017-042BJ. Apogee: 461 km (286 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.64 min. See Lemur-2 43 (Lemur-2 ArtFischer). ..

Flock 2k-27 - . Payload: Dove 0F54; FLOCK 2K 27. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42882 . COSPAR: 2017-042BK. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 27 (Dove 0F54). ..

MKA-N 1 - . Payload: MKA-N No. 1. Nation: TBD. USAF Sat Cat: 42834 . COSPAR: 2017-042K. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See MKA-N 1. ..

Flock 2k-46 - . Payload: Dove 103F; FLOCK 2K 46. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42858 . COSPAR: 2017-042AK. Apogee: 457 km (283 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.60 min. See Flock-2k 46 (Dove 103F). ..

Flock 2k-26 - . Payload: Dove 0F53; FLOCK 2K 26. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42883 . COSPAR: 2017-042BL. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 26 (Dove 0F53). ..

Flock 2k-23 - . Payload: Dove 0F4B; FLOCK 2K 23. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42859 . COSPAR: 2017-042AL. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 23 (Dove 0F4B). ..

WNISAT-1R - . Nation: Japan. USAF Sat Cat: 42835 . COSPAR: 2017-042L. Apogee: 605 km (375 mi). Perigee: 585 km (363 mi). Inclination: 97.58 deg. Period: 96.57 min. See WNISAT 1R. ..

MKA-N 2 - . Payload: MKA-N No. 2. Nation: TBD. USAF Sat Cat: 42836 . COSPAR: 2017-042M. Apogee: 604 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See MKA-N 2. ..

Flock 2k-25 - . Payload: Dove 0F4D; FLOCK 2K 25. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42884 . COSPAR: 2017-042BM. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 25 (Dove 0F4D). ..

Flock 2k-21 - . Payload: Dove 0F49; FLOCK 2K 21. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42860 . COSPAR: 2017-042AM. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 21 (Dove 0F49). ..

Lemur-2-Greenberg - . Payload: Lemur-2-42; LEMUR 2 GREENBERG. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42837 . COSPAR: 2017-042N. Apogee: 602 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.53 min. See Lemur-2 42 (Lemur-2 Greenberg). ..

Flock 2k-20 - . Payload: Dove 0F47; FLOCK 2K 20. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42885 . COSPAR: 2017-042BN. Apogee: 459 km (285 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 20 (Dove 0F47). ..

Flock 2k-22 - . Payload: Dove 0F4A; FLOCK 2K 22. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42861 . COSPAR: 2017-042AN. Apogee: 455 km (282 mi). Perigee: 442 km (274 mi). Inclination: 96.96 deg. Period: 93.55 min. See Flock-2k 22 (Dove 0F4A). ..

Lemur-2-AndiS - . Payload: Lemur-2-47; LEMUR 2 ANDIS. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42838 . COSPAR: 2017-042P. Apogee: 602 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.53 min. See Lemur-2 47 (Lemur-2 AndiS). ..

Flock 2k-7 - . Payload: Dove 0F2B; FLOCK 2K 07. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42862 . COSPAR: 2017-042AP. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 7 (Dove 0F2B). ..

Flock 2k-19 - . Payload: Dove 0F46; FLOCK 2K 19. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42886 . COSPAR: 2017-042BP. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 19 (Dove 0F46). ..

Flock 2k-18 - . Payload: Dove 0F44; FLOCK 2K 18. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42887 . COSPAR: 2017-042BQ. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 18 (Dove 0F44). ..

Lemur-2-Monson - . Payload: Lemur-2-44; LEMUR 2 MONSON. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42839 . COSPAR: 2017-042Q. Apogee: 603 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.54 min. See Lemur-2 44 (Lemur-2 Monson). ..

Flock 2k-8 - . Payload: Dove 0F2D; FLOCK 2K 08. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42863 . COSPAR: 2017-042AQ. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 8 (Dove 0F2D). ..

Flock 2k-17 - . Payload: Dove 0F40; FLOCK 2K 17. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42888 . COSPAR: 2017-042BR. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 17 (Dove 0F40). ..

Flock 2k-5 - . Payload: Dove 0F29; FLOCK 2K 05. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42864 . COSPAR: 2017-042AR. Apogee: 456 km (283 mi). Perigee: 442 km (274 mi). Inclination: 96.96 deg. Period: 93.57 min. See Flock-2k 5 (Dove 0F29). ..

Lemur-2-Furiaus - . Payload: Lemur-2-45; LEMUR 2 FURIAUS. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42840 . COSPAR: 2017-042R. Apogee: 602 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.53 min. See Lemur-2 45 (Lemur-2 Furiaus). ..

Flock 2k-16 - . Payload: Dove 0F3D; FLOCK 2K 16. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42889 . COSPAR: 2017-042BS. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 16 (Dove 0F3D). ..

Flock 2k-40 - . Payload: Dove 1053; FLOCK 2K 40. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42865 . COSPAR: 2017-042AS. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 40 (Dove 1053). ..

Lemur-2-PeterG - . Payload: Lemur-2-48; LEMUR 2 PETERG. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42841 . COSPAR: 2017-042S. Apogee: 601 km (373 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.52 min. See Lemur-2 48 (Lemur-2 PeterG). ..

Flock 2k-39 - . Payload: Dove 1052; FLOCK 2K 39. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42866 . COSPAR: 2017-042AT. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 39 (Dove 1052). ..

Flock 2k-15 - . Payload: Dove 0F3C; FLOCK 2K 15. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42890 . COSPAR: 2017-042BT. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 15 (Dove 0F3C). ..

Lemur-2-Dembitz - . Payload: Lemur-2-49; LEMUR 2 DEMBITZ. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42842 . COSPAR: 2017-042T. Apogee: 601 km (373 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.51 min. See Lemur-2 49 (Lemur-2 Dembitz). ..

Flock 2k-37 - . Payload: Dove 1050; FLOCK 2K 37. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42867 . COSPAR: 2017-042AU. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 37 (Dove 1050). ..

CICERO-1 - . Nation: TBD. USAF Sat Cat: 42843 . COSPAR: 2017-042U. Apogee: 603 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.54 min. See CICERO 1. ..

Flock 2k-13 - . Payload: Dove 0F37; FLOCK 2K 13. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42891 . COSPAR: 2017-042BU. Apogee: 457 km (283 mi). Perigee: 442 km (274 mi). Inclination: 96.96 deg. Period: 93.58 min. See Flock-2k 13 (Dove 0F37). ..

Flock 2k-14 - . Payload: Dove 0F3B; FLOCK 2K 14. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42892 . COSPAR: 2017-042BV. Apogee: 459 km (285 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 14 (Dove 0F3B). ..

NanoACE - . Nation: USA. USAF Sat Cat: 42844 . COSPAR: 2017-042V. Apogee: 601 km (373 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.52 min. See NanoACE. ..

Flock 2k-38 - . Payload: Dove 1051; FLOCK 2K 38. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42868 . COSPAR: 2017-042AV. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 38 (Dove 1051). ..

Flock 2k-31 - . Payload: Dove 104A; FLOCK 2K 31. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42869 . COSPAR: 2017-042AW. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 31 (Dove 104A). ..

Flock 2k-12 - . Payload: Dove 0F36; FLOCK 2K 12. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42893 . COSPAR: 2017-042BW. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 12 (Dove 0F36). ..

Lemur-2-Zachary - . Payload: Lemur-2-46; LEMUR 2 ZACHARY. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42845 . COSPAR: 2017-042W. Apogee: 601 km (373 mi). Perigee: 581 km (361 mi). Inclination: 97.58 deg. Period: 96.50 min. See Lemur-2 46 (Lemur-2 Zachary). ..

Landmapper-BC2 - . Payload: Corvus-BC 2; CORVUS BC2. Nation: USA. USAF Sat Cat: 42846 . COSPAR: 2017-042X. Apogee: 599 km (372 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.52 min. See Landmapper-BC 2 (Corvus-BC 2). ..

Flock 2k-11 - . Payload: Dove 0F33; FLOCK 2K 11. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42894 . COSPAR: 2017-042BX. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 11 (Dove 0F33). ..

Flock 2k-32 - . Payload: Dove 104B; FLOCK 2K 32. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42870 . COSPAR: 2017-042AX. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 32 (Dove 104B). ..

Flock 2k-10 - . Payload: Dove 0F32; FLOCK 2K 10. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42895 . COSPAR: 2017-042BY. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 10 (Dove 0F32). ..

Landmapper-BC1 - . Payload: Corvus-BC 1; CORVUS BC1. Nation: USA. USAF Sat Cat: 42847 . COSPAR: 2017-042Y. Apogee: 599 km (372 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.51 min. See Landmapper-BC 1 (Corvus-BC 1). ..

Flock 2k-29 - . Payload: Dove 1048; FLOCK 2K 29. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42871 . COSPAR: 2017-042AY. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 29 (Dove 1048). ..

Flock 2k-30 - . Payload: Dove 1049; FLOCK 2K 30. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42872 . COSPAR: 2017-042AZ. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 30 (Dove 1049). ..

CICERO-2 - . Nation: TBD. USAF Sat Cat: 42848 . COSPAR: 2017-042Z. Apogee: 597 km (370 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.50 min. See CICERO 2. ..

Flock 2k-9 - . Payload: Dove 0F2E; FLOCK 2K 09. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42896 . COSPAR: 2017-042BZ. Apogee: 456 km (283 mi). Perigee: 441 km (274 mi). Inclination: 96.96 deg. Period: 93.56 min. See Flock-2k 9 (Dove 0F2E). ..

Flock 2k-42 - . Payload: Dove 1055. Nation: USA. Spacecraft: Cubesat. COSPAR: 2017-042Z. See Flock-2k 42 (Dove 1055). ..

Flock 2k-6 - . Payload: Dove 0F2A; FLOCK 2K 06. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42897 . COSPAR: 2017-042CA. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 6 (Dove 0F2A). ..

Flock 2k-44 - . Payload: Dove 1020; FLOCK 2K 44. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42873 . COSPAR: 2017-042BA. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 44 (Dove 1020). ..

CICERO-3 - . Nation: TBD. USAF Sat Cat: 42849 . COSPAR: 2017-042AA. Apogee: 597 km (370 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.49 min. See CICERO 3. ..

2017 October 14 - . 08:45 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Progress MS-07 - . Payload: Progress 7K-TGM No. 437. Nation: Russia. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Progress MS. USAF Sat Cat: 42971 . COSPAR: 2017-065A. Apogee: 435 km (270 mi). Perigee: 383 km (237 mi). Inclination: 51.64 deg. Period: 92.75 min. See Progress-MS 07. ..

2018 February 1 - . 02:06 GMT - . Launch Site: Vostochniy. Launch Complex: Vostochniy PU1S. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Kanopus-V No. 3 - . Payload: Kanopus-V; KANOPUS-V 3. Nation: Russia. USAF Sat Cat: 43180 . COSPAR: 2018-014A. Apogee: 510 km (310 mi). Perigee: 508 km (315 mi). Inclination: 97.45 deg. Period: 94.80 min. See Kanopus-V 3. ..

Kanopus-V No. 4 - . Payload: Kanopus-V; KANOPUS-V 4. Nation: Russia. USAF Sat Cat: 43181 . COSPAR: 2018-014B. Apogee: 510 km (310 mi). Perigee: 508 km (315 mi). Inclination: 97.45 deg. Period: 94.80 min. See Kanopus-V 4. ..

Lemur-2-Jin-Luen - . Payload: Lemur-2-74; LEMUR 2 JIN-LUEN. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43182 . COSPAR: 2018-014C. Apogee: 590 km (360 mi). Perigee: 568 km (352 mi). Inclination: 97.71 deg. Period: 96.25 min. See Lemur-2 76 (Lemur-2 Jin-Luen). ..

Lemur-2-UramChanSol - . Payload: Lemur-2-75; LEMUR 2 URAMCHANSOL. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43183 . COSPAR: 2018-014D. Apogee: 590 km (360 mi). Perigee: 568 km (352 mi). Inclination: 97.71 deg. Period: 96.25 min. See Lemur-2 77 (Lemur-2 UramChanSol). ..

Lemur-2-Kadi - . Payload: Lemur-2-76; LEMUR 2 KADI. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43184 . COSPAR: 2018-014E. Apogee: 590 km (360 mi). Perigee: 568 km (352 mi). Inclination: 97.71 deg. Period: 96.24 min. See Lemur-2 74 (Lemur-2 Kadi). ..

Lemur-2-TheNickMolo - . Payload: Lemur-2-77; LEMUR 2 THENICKMOLO. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43185 . COSPAR: 2018-014F. Apogee: 589 km (365 mi). Perigee: 568 km (352 mi). Inclination: 97.71 deg. Period: 96.25 min. See Lemur-2 75 (Lemur-2 TheNickMolo). ..

S-NET 1 - . Nation: Germany. USAF Sat Cat: 43186 . COSPAR: 2018-014G. Apogee: 586 km (364 mi). Perigee: 569 km (353 mi). Inclination: 97.72 deg. Period: 96.22 min. See S-Net A (Tubsat 13). ..

S-NET 2 - . Nation: Germany. USAF Sat Cat: 43187 . COSPAR: 2018-014H. Apogee: 586 km (364 mi). Perigee: 569 km (353 mi). Inclination: 97.72 deg. Period: 96.22 min. See S-Net B (Tubsat 14). ..

S-NET 3 - . Nation: Germany. USAF Sat Cat: 43188 . COSPAR: 2018-014J. Apogee: 586 km (364 mi). Perigee: 569 km (353 mi). Inclination: 97.72 deg. Period: 96.22 min. See S-Net C (Tubsat 15). ..

S-NET 4 - . Nation: Germany. USAF Sat Cat: 43189 . COSPAR: 2018-014K. Apogee: 586 km (364 mi). Perigee: 569 km (353 mi). Inclination: 97.72 deg. Period: 96.22 min. See S-Net D (Tubsat 16). ..

D-Star One v1.1 Phoenix - . Payload: D-Star One. Nation: Germany. COSPAR: 2018-014L. See D-Star ONE v.1.1 Phoenix. ..

2018 February 13 - . 08:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Progress MS-08 - . Payload: Progress 7K-TGM No. 438. Nation: Russia. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Progress MS. USAF Sat Cat: 43211 . COSPAR: 2018-019A. Apogee: 401 km (249 mi). Perigee: 346 km (214 mi). Inclination: 51.64 deg. Period: 92.02 min. See Progress-MS 08. ..

2018 July 9 - . 21:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.

Progress MS-09 - . Payload: Progress 7K-TGM No. 439. Nation: Russia. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Progress MS. USAF Sat Cat: 43537 . COSPAR: 2018-058A. Apogee: 411 km (255 mi). Perigee: 404 km (251 mi). Inclination: 51.64 deg. Period: 92.71 min. See Progress-MS 09. ..

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