Year of Launch 2015 rae table of Earth Satellites (Issued 2015) Page
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$ DArke Matter Particle Explorer can measure the direction, energy and electric charge of particles for the continued search for dark matter. Galileo 12 (269) 2015 79 A 2015 Dec 17.494 Box +2 panels 2.5 x 1.2 2015 Dec 17.74 54.96 859.85 29953 23550 23599 0.0008 190 [Soyuz 2-1B/Fregat] [41174] 1 million years 717 x 1.1 2015 Dec 18.62 54.96 859.22 29939 23540 23580 0.0006 146 (VS13) KOU-ELS 14.67 span 2015 Dec 19.43 54.96 859.23 29939 23539 23582 0.0007 146 2015 Dec 21.39 54.95 858.33 29918 23511 23568 0.001 192
[41175] 1 million years 717 x 1.1 2015 Dec 17.75 54.96 860.50 29969 23557 23622 0.001 215 14.67 span 2015 Dec 18.61 54.96 860.28 29963 23552 23617 0.001 204
Fregat MT 2015 79 C 2015 Dec 17.494 Spheres 1.5 long 2015 Dec 17.74 54.98 858.62 29925 23515 23577 0.001 138 Upperstage [41176] + nozzle 3.35 dia 2015 Dec 18.60 54.97 859.37 29942 23533 23593 0.001 194 1050
D Progress MS-01 & 2015 80 A 2015 Dec 21.364 Cyl+beehive+ 7.5 long 2015 Dec 21.74 51.64 90.00 6653 270 279 0.007 270 [Soyuz 2-1A] [41177] 194.962 days +spheroid+ 2.72 maxdia 2015 Dec 22.62 51.61 90.03 6654 268 283 0.001 264 BAI-LC31/6 2016 Jul 3.326 2 panels 2.3 dia 2015 Dec 23.61 51.64 92.60 6780 396 407 0.0008 312 7289
[41178] 1.729 days 2355 2.66 dia 2015 Dec 22.95 51.65 87.40 6524 142 149 0.0005 59 2015 Dec 23.090 % Orbcomm FM 114 2015 81 A 2015 Dec 22.062 Box + panel 1x1x0.5 2015 Dec 22.15 47.00 97.42 7014 613 657 0.003 19 [Falcon 9 v1.1 FT] * [41179] + boom 5 span 2016 Jan 22.93 47.01 97.80 7032 649 659 0.0007 214 CC-LC40 172 8 long
The Progress MS series of spacecraft also carry an improved Kurs rendezvous radar, which feeds range closure rate data to the capsule’s computers during approach to the space station. A radio link with Russian data relay satellites in geostationary orbit is also installed on the new generation of Progress vehicles, allowing communications between the spacecraft and ground controllers even when it is flying outside the range of ground stations on Russian territory, according to Roscosmos, the Russian space agency. The spaceship’s navigation system, space debris shielding and spotlight also see improvements, along with the mechanism that firmly latches the cargo capsule to the space station after docking. Progress MS-01 docked 2015 Dec 23.435 with ISS (Pirs port). On 2016 Jul 1.233 Progress MS-01 undocked from Pirs and separated to a distance of 190 m in a manual undocking and docking test. Re-docked 2016 Jul 1.253 to Pirs. Finally undocked 2016 Jul 3.158 and was de-orbited over the Pacific Ocean. % Decay observed from USA states California, Nevada, Utah and Arizona. * First flight of the upgraded Falcon 9 rocket with longer 1st stage tanks, longer 2nd stage, super cooled and densified liquid oxygen, higher trust engines. The 1st stage made a successful return and soft landing at Cape Canaveral on Landing Zone 1, the formerly LC13. Orbcomm FM 119 2015 81 B 2015 Dec 22.062 Box + panel 1x1x0.5 2015 Dec 22.15 47.00 97.42 7014 613 657 0.003 20 [41180] + boom 5 span 2016 Jan 23.78 47.00 97.55 7020 621 663 0.003 177 172 8 long Orbcomm FM 105 2015 81 C 2015 Dec 22.062 Box + panel 1x1x0.5 2015 Dec 22.15 47.00 97.43 7014 614 658 0.003 22 [41181] + boom 5 span 2015 Dec 22.53 47.00 97.42 7013 613 656 0.003 21 172 8 long 2016 Jan 22.10 47.00 97.77 7030 646 658 0.0008 241
[41182] + boom 5 span 2015 Dec 22.53 47.00 97.42 7013 613 656 0.003 21 172 8 long 2016 Jan 22.91 47.00 97.67 7026 637 657 0.001 208
[41183] + boom 5 span 2015 Dec 22.53 47.00 97.42 7013 613 656 0.003 21 172 8 long 2016 Jan 22.90 46.99 97.63 7024 634 657 0.002 172
[41184] + boom 5 span 2015 Dec 22.53 47.00 97.42 7013 613 656 0.003 21 172 8 long
[41185] + boom 5 span 2015 Dec 22.53 47.00 97.38 7012 613 655 0.003 18 172 8 long
[41186] + boom 5 span 2016 Jan 22.94 46.99 97.18 7002 609 639 0.002 175 172 8 long
[41187] + boom 5 span 2015 Dec 22.53 47.00 97.38 7012 612 655 0.003 18 172 8 long 2016 Jan 23.60 47.00 97.02 6994 606 626 0.001 179
[41188] + boom 5 span 2015 Dec 22.46 47.00 97.38 7012 613 654 0.003 17 172 8 long 2016 Jan 22.85 47.01 96.54 6989 603 617 0.001 214
[41189] + boom 5 span 172 8 long Falcon 9 v1.1 FT 2015 81 2015 Dec 22.062 Cylinder 13 long Made a restart after the satellite deployment and decayed over the 2nd stage [NNA] ~4000-4500 3.66 dia Indian Ocean after half an orbit. Ekspress AMU-1 2015 82 A 2015 Dec 24.897 Box +2 panels 7.5 high 2015 Dec 25.54 22.36 712.50 26425 4324 35769 0.595 0 [Proton-M/Breeze-M] [41191] > million years + 4 dishes 2016 Jan 7.69 0.08 1436.12 42165 35786 35787 0.000009 267 BAI-LC200/39 5700 Breeze-M stage 2015 82 B 2015 Dec 24.897 Stubby Cyl 2.62 long 2015 Dec 25.53 23.00 663.83 25208 3680 33979 0.601 3 [41192] 1220 ~2.4 dia Breeze-M tank 2015 82 C 2015 Dec 24.897 Torus 2.1 long 2015 Dec 25.64 49.55 281.93 14244 331 15400 0.529 353 [41193] 1290 4.1 dia 0.8 cross Gaofen-4 * 2015 83 A 2015 Dec 28.670 Hexagonal box 2015 Dec 28.75 22.97 631.57 24384 205 35806 0.730 180 [CZ-3B/E] [41194] > million years + cylinder 2016 Jun 7.94 0.58 1436.07 42164 35784 35787 0.00004 20 XI +2 panels 2016 Jun 16.51 0.57 1436.13 42166 35785 35789 0.00004 41 4700 2016 Jan 22.57 0.56 1436.03 42164 35783 35788 0.00007 359 CZ-3B/E 3rd stage 2015 83 B 2015 Dec 28.670 Cylinder 12.38 long 2015 Dec 28.76 22.97 603.47 23656 162 34392 0.723 179 [41195] 2740 3 dia * First Chinese geostationary remote sensing satellite.
Dragon CRS-5 Solar Panel Covers; 2 pieces, both have decayed D 2015 01 B [40371] 2015 Jan 13 3 days 2015 Jan 10.41 51.65 90.12 6659 205 356 0.011 47 2015 Jan 12.83 51.62 88.22 6565 162 210 0.004 50 D 2015 01 C [40372] 2015 Jan 12 2 days 2015 Jan 10.41 51.66 90.12 6659 206 354 0.011 47 2015 Jan 12.29 51.62 89.00 6603 183 267 0.006 48 GPS IIF-9 Delta 4 2nd stage fragments; 3 pieces, all in orbit D 2015 13 C [40597] 2015 Apr 23 31 days 2015 Apr 23.63 52.02 112.42 7716 195 2480 0.148 103 2015 13 D [40598] 2015 13 E [40599] Breeze KM stage fragments; 6 pieces, all in orbit 2015 20 F [41718] 2016 Jul 26.40 82.49 111.52 7675 1121 1472 0.023 214 2015 20 G [41719] 2016 Jul 27.66 82.49 112.93 7740 1189 1533 0.022 220 2015 20 H [41720] 2016 Jul 24.42 82.49 111.55 7676 1121 1474 0.023 219 2015 20 J [41721] 2016 Jul 23.45 82.49 112.97 7742 1173 1553 0.025 229 2015 20 K [41722] 2016 Jul 26.42 82.49 113.35 7759 1241 1519 0.018 227 2015 20 L [41723] 2016 Jul 23.42 82.49 111.48 7674 1124 1466 0.022 222 Dragon CRS-6 Solar Panel Covers; 2 pieces, both have decayed 2015 21 C [40590] 2015 Apr 14.86 51.66 90.20 6663 205 363 0.012 48 2015 21 D [40591] 2015 Apr 14.92 51.67 90.10 6658 203 356 0.012 47 Progress-M 27M and Soyuz-2 1A 3rd stage fragments; 20 pieces, 13 have decayed D 2015 24 C [40621] 2015 Apr 29 1 day 2015 Apr 28.67 51.62 89.55 6630 164 340 0.013 103 D 2015 24 D [40622] 2015 Apr 29 1 day 2015 Apr 28.66 61.51 88.83 6595 152 281 0.010 51 D 2015 24 E [40623] 2015 Apr 29 1 day 2015 Apr 28.79 51.61 89.03 6605 177 276 0.008 94 D 2015 24 F [40624] 2015 Apr 29 1 day 2015 Apr 28.60 51.65 88.15 6562 165 201 0.003 56 D 2015 24 G [40625] 2015 Apr 29 1 day 2015 Apr 28.78 51.64 88.60 6584 174 237 0.005 89 2015 24 H [40626] 2015 Apr 28.98 51.67 89.88 6648 173 365 0.014 76 D 2015 24 J [40627] 2015 Apr 29 1 day 2015 Apr 28.72 51.63 88.17 6562 154 214 0.005 101 D 2015 24 K [40628] 2015 Apr 29 1 day 2015 Apr 28.78 51.65 87.73 6540 152 174 0.001 47 D 2015 24 L [40629] 2015 Apr 29 1 day 2015 Apr 28.84 51.66 87.62 6535 133 181 0.004 151 D 2015 24 M [40630] 2015 Apr 29 1 day 2015 Apr 28.72 51.67 88.08 6558 168 191 0.002 104 D 2015 24 N [40631] 2015 Apr 29 1 day 2015 Apr 28.60 51.65 88.53 6580 153 251 0.007 142 D 2015 24 P [40632] 2015 Apr 29 1 day 2015 Apr 29.09 51.64 88.33 6571 170 214 0.003 82 2015 Apr 29.64 51.65 87.37 6522 136 152 0.001 87 2015 24 Q [40633] 2015 Apr 29.59 51.64 88.85 6596 180 255 0.006 100 2015 May 1.98 51.64 86.98 6504 114 136 0.002 71 D 2015 24 R [40634] 2015 Apr 29 1 day 2015 Apr 28.84 51.65 88.08 6559 175 185 0.0008 88 2015 24 S [40635] 2015 May 1.55 51.64 88.35 6571 173 212 0.003 90 2015 24 T [40636] 2015 Apr 30.02 51.63 88.42 6575 168 225 0.004 100 D 2015 24 U [40637] 2015 May 7 9 days 2015 Apr 30.98 51.64 89.05 6606 183 272 0.007 99 2015 May 6.73 51.65 87.53 6531 142 163 0.002 122 2015 24 V [40638] 2015 Apr 29.66 51.65 88.28 6569 167 213 0.003 90 2015 24 W [40639] 2015 Apr 29.60 51.63 87.60 6534 143 168 0.002 102 2015 24 X [40640] 2015 May 1.55 51.63 88.03 6556 161 194 0.003 102 Tianhui 1-03 fragment; 3 pieces, all in orbit 2015 61 B [41023] 2015 Nov 6.15 97.33 97.78 7031 499 806 0.022 129 2015 61 C [41024] 2015 Nov 5.78 97.37 98.17 7049 499 843 0.024 135 2015 61 D [41025] 2015 Nov 3.22 97.36 94.48 6872 487 500 0.001 282 Yaogan 28 (*)and CZ-4B fragments; 3 pieces, all in orbit 2015 64 C (*) [41040] 2015 Dec 5.17 97.24 93.93 6846 455 479 0.002 162 2015 64 D [41041] 2015 Dec 4.81 97.27 97.38 7012 469 798 0.023 83 2015 64 E [41042] 2015 Dec 5.32 97.18 97.27 7006 467 789 0.023 86 Yaogan 29 (*) and CZ-4c fragments; 4 pieces, all in orbit 2015 69 C [42670] 2017 Apr 11.19 97.83 95.62 6927 481 616 0.010 140 2015 69 D [42671] 2017 Apr 14.36 97.89 99.02 7091 595 829 0.016 100 2015 69 E [42672] 2017 Apr 13.36 97.95 98.78 7079 584 817 0.016 106 2015 69 F (*) [42673] 2017 Apr 13.76 97.89 96.98 6993 612 616 0.0002 150 Zenit 2nd stage and Fregat JTB fragments; 7 pieces, 2 have decayed. Fragment E-H are the Zenit 2nd stage separation motor covers. 2015 74 E [41109] 2015 Dec 11.91 51.37 94.43 6870 166 817 0.047 66 D 2015 74 F [41110] 2015 Dec 29 18 days 2015 Dec 11.89 51.36 94.48 6872 178 809 0.046 75 2015 Dec 28.45 51.35 88.35 6572 142 244 0.008 133 2015 74 G [41111] 2015 Dec 11.91 51.40 94.63 6879 178 823 0.047 75 2015 74 H [41112] 2015 Dec 11.91 51.40 94.63 6879 165 837 0.049 66 D 2015 74 J [41113] 2017 Nov 13 703 days 2015 Dec 12.00 50.49 132.50 8610 269 4193 0.228 5 2017 Nov 12.40 50.38 89.08 6608 189 269 0.006 95 2015 74 K [41114] 2015 Dec 11.90 50.38 132.45 8608 270 4189 0.228 5 2015 74 L [41115] 2015 Dec 12.02 50.32 132.43 8607 296 4160 0.224 7 Cosmos 2513 Breeze-M stage fragments; 6 pieces, all in orbit 2015 75 D [41543] 2016 May 25.15 0.40 1367.38 40809 33349 35511 0.026 44 2015 75 E [41544] 2016 May 20.91 0.38 1362.58 40714 33120 35549 0.030 27 2015 75 F [41545] 2016 May 5.82 0.37 1363.17 40725 33291 35401 0.026 22 2015 75 G [41546] 2016 May 25.99 0.43 1376.15 40983 33592 35617 0.024 0 2015 75 H [41547] 2016 May 21.04 0.44 1395.45 41365 33843 36130 0.028 334 2015 75 J [41548] 2016 May 22.27 0.86 1409.08 41634 33622 36889 0.039 60 D MexSat-1 2015 F1 2015 May 16.241 Box +2 panels 9 x 3 x 4 The 3th stage of the Proton suffered a malfunction of its RD-0214 steering [Proton-M/Breeze-M] + dish 22 dia engine about 50 sec after lift-off at a height of 160 km. BAI-LC200/39 5325 41 span Debris came down in Kraniy Chikoy some 3400 km from Baikonur. D Dragon CRS-7 2015 F2 2015 Jun 28.598 Blunt cone 4.4 high At 2 min 19 sec after lift-off a tank strut inside the 2nd stage broke off + cylinder 3.66 dia and punctured the oxygen tank, that then exploded CC-LC 40 + 2 panels 2.8 high ruptured. Within 3 sec the Dragon capsule was seen detached from the 8700 full 16.5 span Falcon. After 8 seconds the 1st stage exploded. Debris fell in the Atlantic 2215 cargo Ocean some 150 km NE of Cape Carnaval D HiakaSat * 2015 F3 2015 Nov 4.156 Octagonal cyl 0.647 dia About 58 sec into the flight the 1st stage malfunctioned and the vehicle was [SPARK/Super Strypi] 55 0.403 high destroyed. BS D EDSN # 1.5U Cube 0.17 x 0.10 A total of 8 EDSN satellites were carried. 1.7 x 0.10 D ARGUS % 2U Cube 0.20 x 0.10 3.0 x 0.10 D PrintSat $ 1U Cube 0.10 x 0.10 1 x 0.10
+4 panels x0.365 12 0.84 span D STACEM ^ 3U Cube 0.34 x 0.10 x 0.10
HiakiSat is a technology demonstration satellite and the primary payload for the ORS-4 (Operationally Responsive Space Office)mission with the first flight of the SPARK/Super Strypi rocket launched from the US Navy Pacific Missile Range Facility at Barker Sands, Hawaii. # Edison Demonstration of SmallSat Networks. A loose formation of eight small satellites to demonstrate cross-satellite data communications for flexible data correlation and distribution as well as simplified satellite operations and data downlink. % From St. Louis University and the Institute for Defense and Space Electronics to explore and model the effects of space radiation on modern electronics systems. $ Build by students at Montana Sate University using 3D-printing for the construction of the entire satellite structure. & Supernova-Beta is a prototype satellite built and operated by CubeSat manufacturer Pumpkin Inc. as a demonstration mission of the company’s 6U CubeSat platform. ^ STACEM is a 3-Unit CubeSat designed, built and operated by the Space Dynamics Laboratory, Utah State University Research Foundation. The satellite demonstrates a miniaturized multi-spectral payload for the acquisition of imagery in the visible and near infrared wavelengths and hyperspectral channels. 2016 – Version 1.15 Directory: RAE RAE -> Year of Launch 2009 rae table of Earth Satellites RAE -> [Atlas-v 551] [28928] + antenna 69 high 2006 Mar 87 98 03 Download 491.73 Kb. Share with your friends:
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