Wednesday, November 14, 2018

Girls’ Series Fiction and American Popular Culture

https://welib.org/md5/eff8b05ee222c9e70f76db89fc9de342

Nimiq 2

 2002-062A


Nimiq 2, an A2100AX satellite, used a Proton-M/Briz-M on its first commercial launch. to 91W. Nimiq 1 will be relocated to 82W for backup. In 2003 it was reported that a solar array power problem caused two transponders to be taken off line; the satellite was replaced by Nimiq 1.

Nimiq 2 was leased to Bell Canada until 2013.

Mass 3600 kg.


Nimiq 2 
 

DateTimeEventOrbit  

2002 Dec 29  2316:40 Launch by Proton-M/Briz M  KB 
 2318:42 T+2:02 St 1 sep 
 2322:08 T+5:28 St 2 sep 
 2322:20 T+5:40 Fairing sep
 2326:22 T+9:42 St 3 sep  -1257 x 194 x 51.5 
 2327:55 T+11:15 Briz MES-1 
 2338:26 T+21:46 Briz MECO-1213 x 213 x 51.53  
2002 Dec 30  
 0016:25 T+59:45 Briz MES-2 
 0043:41 T+1:27:01 MECO-2 
 0045:09 T+1:28? DTB Prop tank sep  608 x 17142 x 49.56  
 0045:17 T+1:28:37 MES-3 
 0050:14 T+1:33:34 MECO-3  851 x 35406 x 49.10  
   946 x 35783 x 49.0 (TLE) 
 0551:48 T+6:35:08 MES-4 
 0558:20 T+6:41:48 MECO-4  7904 x 35886 x 16.5 
 0610:00 T+6:53:20 Briz-M sep  
 0858:25 Briz depletion start 
 0858:45 T+9:42 Briz depleted  7872 x 35687 x 16.4 
2002 Dec 30    787.57 7904 x 35886 x 16.49 
2002 Dec 31    929.09 14581 x 35742 x 8.5 
2003 Jan 3    1119.43 22920 x 35748 x 3.8 
2003 Jan 5? LAM 
2003 Jan 10? LAM 
2003 Jan 10    1435.98 35779 x 35789 x 0.1 GEO 82.0W 
2006 Aug 8    1436.12 35779 x 35794 x 0.0 GEO 82.0W 
2008 Oct 24   Move out  GEO 82W 
2008 Nov 3   Move in  GEO 91W 
2013 Sep 5   Move out  1436.09 35777 x 35795 x 0.1 GEO 91.1W 
2013 Sep 20   Move in 72.5W  1435.93 35777 x 35789 x 0.0 GEO 72.5W 
2013 Sep 28    1436.07 35777 x 35794 x 0.0 GEO 72.4W 
2013 Sep 29   Move out, Relocate 39E, HellasSat slot 
2013 Oct 21   Move in 39E  1436.06 35776 x 35794 x 0.0 GEO 39.0E 
2014 Jan 18    1436.05 35762 x 35808 x 0.1 GEO 39.0E 
2014 Jan 26   Orbit move  1453.01 36090 x 36143 x 0.1 GEO 9.9E+4.2W/d 
2014 Feb 15   Braking 
2014 Mar 5   On station 63.0W  1436.08 35775 x 35796 x 0.1 GEO 63.0W 
2014 May 23   Move out  1436.10 35762 x 35811 x 0.1 GEO 63.5W 
2014 Jun 28   Move in 109W  1436.11 35773 x 35800 x 0.0 GEO 109.2W 
2015 Feb 13   Move out from 109W 1436.07 35756 x 35815 x 0.2 GEO 109.1W 
2015 May 5   Move in to GEO 36W  1436.00 35762 x 35806 x 0.4 GEO 36.0W 
  Reserving HispAG1 loc 
2015 Aug 11   Move out  1436.11 35775 x 35798 x 0.6 GEO 36.0W 
2015 Sep 28   Move in , Arabsat 8F? 1435.98 35755 x 35813 x 0.7 GEO 44.4E 
2016 Feb 16    1436.00 35765 x 35803 x 1.0 GEO 44.6E 
2016 Feb 20  Move out 
2016 Mar 27   Move in at 148E 
2016 Apr 1    1436.10 35763 x 35801 x 1.1 GEO 148.1E 
  Testing from Hawaii Pacific Teleport 
2016 Jun 23    1436.16 35769 x 35806 x 1.3 GEO 148.0E 
2016 Jun 24   Move out 
2016 Aug 15   Move in 23.7E  35767 x 35807 x 1.4 GEO 23.7E 
  Slot reservation (Athena-Fidus?) 
2016 Nov 16    1436.06 35779 x 35792 x 1.5 GEO 23.8E 
2016 Nov 16   Move out 
2017 May 7    1446.56 35977 x 36005 x 1.9 GEO 42W+2.6W/d 
2017 May 10  Braking 1443.60 35923 x 35943 x 1.9 GEO 51.5W+1.9W/d 
2017 May 19   Move in at 63.0W  1436.10 35777 x 35796 x 1.9 GEO 63.0W 
  Colocate with Telstar 14R 
2017 Aug 20    1436.13 35769 x 35805 x 2.1 GEO 63.0W 
2017 Aug 22   Move out 
2017 Sep 27   Move in at 90.0E  1436.06 35773 x 35798 x 2.2 GEO 90.0E 
2017 Dec   Adjust to 89.5E 
2018 May 4    1436.09 35764 x 35808 x 2.7 GEO 89.6E 

Friday, October 12, 2018

Meteosat 9

 2005-049B


MSG FM2 was launched in 2005 (originally planned for 2002). It is fully financed by Eumetsat and procured for Eumetsat by ESA. It was built by Alcatel Alenia Space/Cannes.

MSG is below the Sylda 5E and on a 1666V5 adapter with a PSAD anti-shock system and an MFD-C ballast segment. The Sylda 5E is a Sylda 5 extended by 300 mm, for a height of 5.2m.

Launch mass 2034 kg. Size 3.2 dia x 2.3m high.


MSG 2 
 

DateTimeEventOrbit  

2005 Dec 21 2233:00? Launch by Ariane 5GS  
  T+2:20 EAP sep 
  T+3:22 Fairing sep
  T+9:41 EPC MECO 
 2242:47 T+9:47 EPC sep  43.5 x 1701.8 x 6.5 
 2242:54 T+9:54 EPS burn 
 2259:48 T+26:48 EPS MECO 
 2302:05 T+29:05 Insat 4A sep 
 2305:09 T+32:09 Sylda 5 sep 
 2309:32 T+36:32 MSG-2 sep 
2005 Dec 21    671 x 36015 x 3.9 
2005 Dec 25    622 x 35847 x 3.9 
2005 Dec 28    1434.89 35494 x 36031 x 1.8 
2005 Dec 29  0445  Baffle Cover ejected 
 0500  Cooler cover ejected 
2006 Feb 15    1436.09 35783 x 35789 x 1.8 GEO 6.6W 
2007 Feb 6   EW burn  
2007 Apr   Operational 
2015 Nov Op at 9.5e for Rapid Scan service 

Friday, October 5, 2018

GRACE-FO

 2018-047A


JPL/GFZ Grace Follow-On spacecraft pair. Size 1.94m wide x 3.12m long x 0.72m hgh, mass 600 kg.


GRACEFO 
 

DateTimeEventOrbit  

2018 May 22  1947:48  Launch by Falcon 9  V SLC4E 
  T+2:46 MECO 
  T+2:49 St 1 sep 
  T+2:57 SEIG-2 
  T+3:12 Fairing 
 1958:01 T+10:13 SECO-1 
 1959:21 T+11:33 GRACE-FO sep  483 x 504 x 89.0  
 2044:43 T+56:55 SEIG-2 
 2044:51 T+57:03 SECO-2 
 2053:36 T+1:05:48 Irid deploys begin 
 2100:16 T+1:12:28 Irid deploys end  486 x 720 x 86.7 
 2145Stage 2 deorbit 

Ekspress 5

 2002-029A


No. 4 (spacecraft 766 No. Kh001) will replace the Ekspress lost in a Proton failure in 1999. Goes to 14W. Referred to as Ekpress-A1R. mass 2600 kg. The 11S861-01 was used to correct unusually large Proton injection errors.


Ekspress-A1R 
 

DateTimeEventOrbit  

2002 Jun 10  0114:00  Launch by Proton-K/DM-2M  LC200/39 
  Stage 2 sep 
 0124  Stage 3 sep 
 0125? Adapter sep  178 x 185 x 51.6 
 0230? DM-2M 11L burn 1 
  DM-2M MECO-1  185? x 36130? x 47.39  
 0730? DM burn 2 
  SOZ sep 
 0758  DM sep  1454.02 36102 x 36171 x 0.2 GEO 83.1E +4.4W/d 
2002 Jun 13    1454.04 36102 x 36171 x 0.2 GEO 74E-4W/d 
2002 Jun 29   mv in  1435.96 35735 x 35832 x 0.2 GEO 39.2E+0.02E 
2002 Jul 27    1436.03 35776 x 35794 x 0.1 GEO 39.9E 
2005 Sep 2    1436.16 35762 x 35813 x 0.0 GEO 39.8E 
2005 Sep 7   Move out from 40E 
2005 Oct 30   Move in at 14W 
2006 Aug 8    1436.10 35779 x 35793 x 0.1 GEO 14.0W 
2015 Dec 24    1436.13 35763 x 35811 x 5.1 GEO 14.1W 
2015 Dec 25   Move out  1433.24 35707 x 35754 x 5.1 
2016 Mar 10    1430.06 35655 x 35681 x 5.3 GEO 101.4E+1.5E/d

Friday, August 31, 2018

Soyuz MS-09 (Altai)

 2018-051A


Soyuz vehicle 739, mission MS-09 carried Sergei Prokop'ev, Alexander Gerst and Serena Aunon-Chancellor to the International Space Station.


MS09 
 

DateTimeEventOrbit  

2018 Jun 6  1112:39  Launch by Soyuz-FG  KB LC1  
  T+1:54 SAS sep 
  T+1:58 Strapons sep
  T+2:11 52 km alt, 1.8 km/s 
  T+2:23 63 km, 1.9 km/s 
  T+2:42 GO sep 79 km, 2.04 km/s 
  T+2:45 80 km 
 1116 T+4:45 Blok-A MECO 
  T+4:47 Blok-A sep 
  T+4:57 KhO sep 
 1121 T+8:45 Blok-I MECO 
 1121 T+8:48 Blok-I sep  
   88.87 190 x 247 x 51.6 
2018 Jun 6  2000   90.01 273 x 276 x 51.6 
2018 Jun 8    90.04 274 x 279 x 51.6 
 1100   92.66 402 x 407 x 51.6 
 1245? Begin flyaround 
 1250  Lined up for final approach 
 1301  Docked with Rassvet 
 1517  HO to ISS 

Friday, August 24, 2018

Queqiao

 2018-045A


Chang'-e 4 Relay satellite at EML2 halo orbit.


C4R 
 

DateTimeEventOrbit  

2018 May 20  2128:50 Launch by CZ-4C Y27  Xichang 
  T+2:32 St 1 sep 
  T+2:34 St 2 burn 
  T+4:04 Fairing 
  T+4:53? St 2 sep? 
  Stage 3 burn 
 2138 T+9:20? St 3 MECO-1 
 2150 T+22:01 Stage 3 burn 2 
 2152  T+24:01? Stage 3 MECO 2 
 2154? T+25:31? QQ sep from Stage 3  200 x 400000 
 2155? Subsats sep from stage 3 
2018 May 21 1300 Pass EL1:4  159 x 376347 x 29.0  
2018 May 24  2004  St3 in L sphere 
 2037  QQ in L sphere 
2018 May 25  1330  Approaching perilune  100 x -16370 x 16.5 
 1332  Braking burn  
 1340 Lunar flyby 100 km 
 1403  Stage 3 lunar flyby 9882 km  9832 x -25961 x 171.9 
2018 May 26  0804  St3 depart L sphere 
2018 May 30   Stage 3 orbit  16911 x 442890 x 14.5 
2018 May 28?   QQ reach L sphere at EML2 
2018 Jun 14  0306  EML2 Halo orbit insertion

Interkosmos: The Eastern Bloc's Early Space Program

 https://welib.org/md5/66fc3f7cc6b6a9b0f1a33db42cff24e7

Friday, August 17, 2018

SES-12

 2018-049A


SES-12 is an Airbus Eurostar E3000 satellite located at 95E.


SES 12 
 

DateTimeEventOrbit  

2018 Jun 4 0445 Launch by Falcon 9 1040.2 CC SLC40 
  T+2:44 MECO 
  T+2:48 St 1 sep 
  T+2:55 SES-1 
  T+3:37 Fairing 
 0453:25 T+8:25 SECO-1 
 0511:06 T+26:06 SES-2 
 0512:13 T+27:13 SECO-2 
 0517:14 T+32:14 Stage 2 sep 
2018 Jun 4    1118.51 246 x 58384 x 26.0 

Thursday, August 16, 2018

Apstar 6

 2005-012A


Alcatel Space Spacebus 4000C2 replacement for Apstar 1A. at 134E. TV broadcasting in China. Mass 4680 kg.


Apstar 6 
 

DateTimeEventOrbit  

2005 Apr 12  1200  Launch by CZ-3B  XSC 
  T+2:07? Booster sep 
  T+2:27? St 1 sep 
  T+3:52? Fairing sep
  T+5:32? St 2 sep 
  T+5:32? St 3 MES-1 
 1210 T+10:31? MECO-1  160? x 450? x 28.5? 
 1221  T+21:21? MES-2 
 1224 T+24:20? MECO-2 
 1225 Stage 3 sep  209 x 49991 km x 26  
2005 Apr 22    1434.60 35721 x 35792 x 0.1 GEO 141.5E+0.37E 
2005 May 6    1436.12 35780 x 35793 x 0.0 GEO 141.9E-0.01W 
2005 Jul 13    1436.12 35778 x 35796 x 0.0 GEO 134.0E 
2006 Aug 8    1436.14 35779 x 35794 x 0.0 GEO 134.0E 
2018 May 27   Solar array problem 
2018 Jul 1    1436.10 35776 x 35797 x 0.0 GEO 133.9E 

Wednesday, August 15, 2018

Al Yah 3

 2018-012B


Yahsat satellite with Ka-band payload. Orbital Geostar-3.

Flight VA241 took off on time, but headed on entirely the wrong launch azimuth, and the rocket delivered the payloads to a 20 degree inclination orbit instead of the planned 3 degree one. Because of the incorrect trajectory, ground controllers lost telemetry around the time of ESC-A ignition, leading to fears the mission was entirely lost - but the satellites were later found in orbits with the correct apogee and perigee, and the wrong inclination.

The investigation report confirms that a single wrong number was responsible for the incorrect orbit achieved by Ariane V241/L5101. The inertial reference system was aligned at the usual 90 degrees azimuth, but for this mission - targeted at a slightly different transfer orbit than usual - 70 degrees should have been specified.


SES-14 
 

DateTimeEventOrbit  

2018 Jan 25  2220  Launch by Ariane 5ECA L5101  CSG ELA3 
  T+0:07 Liftoff 
  T+2:19 EAP sep 
  T+3:18 Fairing sep
  T+8:51 EPC MECO 
  T+8:58 EPC sep 
 2229 T+9:01 ESC-A burn 
 2244 T+24:46 ESC-A MECO 
 2247 T+27:05 SES-14 sep 
 2253 T+33:22 SYLDA sep 
 2255 T+35:07 Al Yah 3 sep 
2018 Jan 26    780.28 231 x 43164 x 20.7 
2018 Feb 1  1540  LAM-1, at apogee 48 m/s ?  789.42 677 x 43155 x 20.0 
2018 Feb 7  0807  LAM-2 at 34000 km 528 m/s?  1009.90 6141 x 47790 x 21.5  
2018 Feb 10  1245  LAM 3 at 44170 km 631 m/s? 1202.1 14973 x 47192 x 9.3 
2018 Feb 13  0051  LAM4 at 44000 km 266 m/s? 1350.92 20923 x 47281 x 6.2  
2018 Feb 15    1348.08 20828 x 47263 x 6.2 
2018 Feb 15    1415.75 23343 x 47524 x 5.6 
2018 Feb 22    1415.75 23344 x 47430 x 5.5 GEO 150.9W + 5.2E/d 
2018 Feb 27    1440.46 24245 x 47499 x 5.2 
2018 Mar 5    1447,44 255225 x 46792 x  
2018 Mar 16    1452.53 27504 x 44710 x 3.8 GEO 158.5W-4.1W/d 
2018 Apr 13    1454.68 33757 x 38541 x 1.1 
2018 Apr 24    1439.92 35855 x 35867 x 0.1 GEO 14.4W+1.0W/d 
2018 Apr 30    1438.78 35812 x 35866 x 0.1 GEO 19.3W+0.7W/d 
2018 May 2   On station  1436.10 35780 x 35792 x 0.1 GEO 20.1W 
2018 May 9    1436.11 35783 x 35791 x 0.0 GEO 20.1W 
2018 Jun 7    1436.05 35777 x 35794 x 0.0 GEO 20.1W 

November 20,2006

  https://en.wikipedia.org/wiki/Association_football