Saturday, December 26, 2015

Beidou 13

 2011-038A


CALT called the satellite Beidou-2 IGSO-4 (Beidou er hao IGSO-4 weixing). The Xinhua news agency mostly refers to it as 9th Beidou Navigation Satellite (di jiu ke Beidou daohang weixing) although it does also describe it as 'Beidou daohang xitong (Compass Navigation System) zu wang (networking) de di si ke (4th) qingxidei (inclined) qiu (geo) tongbu (synchronous) guidao (orbit) weixing (satellite)'. I will use the 'Beidou daohang weixing 9' or 'Beidou DW9' for short, as a reasonable English-alphabet rendering of the name used by Xinhua.


BDW9 
 

DateTimeEventOrbit  

2011 Jul 26  2144 Launch by CZ-3A XSC 
  T+2:25? Stage 1 MECO 
  T+2:27? Stage 2 MES, Stage 1 sep 
  T+3:52? Fairing sep
  T+4:15? St 2 MECO 
  T+4:20? St 2 VECO 
  T+4:21? St 2 sep, St 3 MES-1 
 2154? T+10? St 3 MECO  190? x 450 ? x 55.1 
 2157? St 3 MES-2 
 2157  Perigee 
 2158? St 3 MECO-2 
 2158? T+14? St 3 sep  
2011 Jul 27    629.87 195 x 35729 x 55.05 
2011 Aug 4    1436.02 35699 x 35870 x 55.2 GEO/T 90.6E 
2013 May 1    1435.90 35687 x 35877 x 54.9 GEO/T 80.3E 

July 10,2006

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

Friday, December 25, 2015

Space Shuttle Discovery: The Champion of the Space Shuttle Fleet

 https://welib.org/md5/2f56daaf139fbcefabc1bda4d0872196

Nimiq 6

 2012-026A


Telesat Ku-band satellite, capacity to be leased to Bell Canada. Loral 1300 satellite, stationed at 91W.

Mass 4745 kg.


N6 
 

DateTimeEventOrbit  

2012 May 17  1912:14  Launch by Proton 93529/99530  KB LC81/24 
 1914:13 St 1 sep 
 1917:41  St 2 sep 
 1917:59  GO sep 
 1921:56  St 3 MECO -495 x 171 x 51.5 
 1921:56  OB/St 3 sep 
 1923:30  MDU-1 
 1927:56  MECO-1  172 x 173 x 51.55  
 1933?  Stage 3 entry 
 2019:44  MDU-2 
 2037:30  MECO-2  270 x 4997 x 50.35  
 2240:58  MDU-3 
 2256:28  MECO-3 
 2257:18  DTB sep  353 x 24910 x 49.3  
 2258:45  MDU-4 
 2300:55  MECO-4  410 x 35767 x 49.1  
2012 May 18 
 0403:04  MDU-5 
 0413:00  MECO-5  12073 x 35786 x 10.2  
 0426:14  Briz-M sep 
 0628:54  SOZ-7 
 0738:54  SOZ-8 cutoff 
2012 May 18    873.03 11985 x 35775 x 10.2 
2012 May 19    1084.34 21399 x 35769 x 4.3 
2012 May 21    1412.56 34893 x 35755 x 0.3 
2012 May 22    1430.61 35607 x 35750 x 0.1 dr past 6E 
2012 May 28   On sta 138W  1436.04 35777 x 35793 x 0.0 GEO 138.0W 
2012 May 31   Depart 138W 
2012 Jun 8    1416.61 35379 x 35429 x 0.0 GEO 106.8W+5.0E/d 
2012 Jun 19   GEO 91W  1436.09 35763 x 35809 x 0.0 GEO 91.1W 
2013 Jun 6    1436.11 35774 x 35799 x 0.0 GEO 91.1W 

Thursday, December 24, 2015

Panamsat 10

 2001-019A


HS-601HP 'Panamsat International Satellite', for launch 2001. At 68.5E. The satellite is 3772 kg launch. 26.2m span, 7.0m high deployed. PAS-10 replaces PAS-4 (which suffered an SCP failure) in the IOR location, broadcasting TV channels to Africa, Europe and Asia.


PAS 10 
 

DateTimeEventOrbit  

2001 May 15  0111:30 Launch by Proton 403-01 LC81/23 
  T+2:00 St 2 burn 
  T+2:06 St 1 sep 
  T+5:34 St 2 MECO 
  T+5:35 St 2 sep 
  T+5:40 St 3 MES 
  T+5:44 Fairing sep
  T+9:38 St 3 MECO 
 0121:19 T+9:49 St 3 sep 
 0121  Adapter sep  129 x 166 x 51.6  
 0225:49 T+1:14:19 DM3 No. 6L MES-1 
 0232:22  T+1:20:52DM MECO-1   
2001 May 15    636.07 205 x 36039 x 51.5 
 0730:25  T+6:18:55 DM MES-2 
 0732:15 T+6:20:45 DM MECO-2 
 0744  (T+6:40:32s) S/c sep  7150 x 36000 x 17.05 (s) 
2001 May 15    774.85 7155 x 35979 x 17.0 
  LAM-1 
2001 May 17    870.12 11604 x 36022 x 11.0 
2001 May 18   LAM-2 1193.81 26043 x 35755 x 2.3 
2001 May 20?   LAM-3 
2001 May 22    1436.53 35771 x 35820 x 0.1 
2001 Jun 9    1436.05 35703 x 35868 x 0.0 GEO 72.0E 
2001 Jul 14   Relocate to 68.5E 
2001 Aug 29    1436.09 35784 x 35788 x 0.0 GEO 68.5E 
2006 Aug 3    1436.10 35777 x 35795 x 0.0 GEO 68.5E 
2012 Oct 25    1436.08 35776 x 35795 x 0.1 GEO 68.5E 

Rich Kids of Instagram

https://welib.org/md5/44d547b226a14ce46fcb8bddf2a9adef

Suburgatory

https://welib.org/md5/a2d76ce69220c8db2b21873ff6a50719

Jem and the Holograms : ultimate handbook

 https://welib.org/md5/4e87d58e03babb1a5967fda9ce457aee

Wednesday, December 23, 2015

Aquarius

 2011-024A


NASA/CONAE Aquarius/SAC-D satellite launch by Delta for measurements of sea surface salinity, makes 0.2 psu global salinity maps every month. Bus is SAC-C derived. Oct cyl + 2 panels + dish, 3 x 6 x 4m. Managed by JPL; after commissioning, the Aquarius radiometer will be managed by GSFC. PI is Gary Lagerloef, Earth and Space Research (ESR/Seattle); SAC-D PI is Sandra Torrusio of CONAE.

Launch by Delta 7320-10C from VAFB. Control from Tabanera Space Center in Cordoba province. 1642 kg (launch configuration of 2.74 m x 4.85 m)


 
 

DateTimeEventOrbit  

2011 Jun 10 1420:13 Launch by Delta 7320-10C  VAFB SLC2W 
  T+1:04 SRM burnout 
  T+1:39 SRM sep 
  T+4:24 MECO 
  T+4:32 Stage 1 sep 
 1424 T+4:38 SES-1 
  T+4:50 Fairing, 130 km 
 1431 T+11:16 SECO-1  157 x 669  
 1512 T+52:19 SES-2 
 1512 T+52:32 SECO-2 
 1516 T+56:42 Stage 2 sep 
  T+1:26:40 SES-3 evasive 
  T+1:25:45 SECO-3 
  T+1:43:20 SES-4 depletion 
  T+1:43:42 SECO-4 
2011 Jul 4 T+25d deploy reflector 
2015 Jun 7  end of ops

Payload:

  • Aquarius L-band 1.26GHz scatterometer/1.41 GHz radiometer (JPL/ESR/GSFC/Lagerloef)

  • MWR Microwave radiometer (CONAE/IAR/)

Tuesday, December 22, 2015

MESSENGER

 2004-030A


Selected as Discovery mission 1999 Jul.

The Mercury Surface, Space Environment, Geochemistry and Ranging mission will be a Mercury orbiter (S. Solomon/Carnegie-DC). Built and managed by APL with SOC at APL.

Mass 1130 kg, 513 kg dry. Spacecraft is 1.42m tall, 1.85m wide and 1.27m deep with a 2.5 x 2.0m front-mounted sunshade and a 6.0-m span pair of solar panels, and 3.6-m mag boom.

MESSENGER will study the geology of Mercury's surface, its magnetic field, and its gravity field.

The initial insertion was about 2 sigma off; target insertion B-plane miss for Earth-1 was about 0.2M km but actual value was 2.3Mkm (OD003, Williams et al 2005). Hence, the third stage did not reenter the Earth gravisphere during Earth-1.

 


Messenger 
 

DateTimeEventOrbit  

2004 Aug 3  0615:56 Launch by Delta 7925H  CC SLC17B 
  T+1:21 SRM 1-6 sep 25 km 
  T+2:40 SRM 7-9 sep 67 km  
 0620:20 T+4:24 MECO 114.7 km 
  Thor sep 
 0620:33 T+4:37 SES-1 121 km 6.1 km/s rel 
 0620 T+4:41 9.5-foot fairing sep 122.9 km 6.2 km/s rel 
 0624:45 T+8:49 SECO-1 169.2 km 7.404 km/s rel  165 x 169 x 32.44 
 0701:57 T+46:01 SES-2  
 0704:48 T+48:52 SECO-2  156 x 7661 x 32.49  
 0705:31 T+49:35 Stage 2 sep 
 0706:10 T+50:14 TES  
 0707:35 T+51:39 TECO 260.3 km 11.297 km/srel 
  T+56:39 Yo-yo despin 
 0712:39 T+56:43 Stage 3 sep 
 0756  T+1:40:00 SES-3 
 0756  T+1:40:24 SECO-3 depletion  171.38 158 x 7529 x 32.2 
 0810   190 x -61706 x 32.7  
 1459  Pass EL1:4 
 1900   194 x -61724 x 32.7 
2004 Aug 4  0600  Pass lunar orbit 
2004 Aug 5  1800  Leave Earth SOI 
2004 Aug 7  0758  Depart Earth sphere 1.5Mkm 
2004 Aug 9  2300   365.93d 0.9248 x 1.076 AU x 6.40 
2004 Aug 24  2100:00  TCM-1 3:36, 18m/s  
2004 Sep 24  1600:00  TCM-2 62s 4.6m/s 
2004 Nov 18  1930  TCM-3 48s 3.2m/s, reduce vel 
2005 Jun 10    365.35d 0.9234 x 1.0769 AU x 6.35  
2005 Jun 23  1430  TCM-5 1.1m/s 174s  
2005 Jul 21  1800  TCM-6 0.1m/s 23s   
2005 Jul 29  1835  Enter Earth Sphere 1.5Mkm 
2005 Jul 31  0800  Enter Earth SOI 
2005 Aug 1  2000  Pass lunar orbit 
2005 Aug 2  1913  Earth-1 flyby 2347 km over Mongolia  2336 x -63487 x 133.1 
2005 Aug 3  1800  Pass lunar orbit 
2005 Aug 5  0600  Leave Earth SOI 
2005 Aug 6  1955  Depart Earth Sphere 1.5Mkm 
2005 Aug 29    265.63d 0.6022 x 1.0152AU x 2.53  
2005 Dec 12 1130 DSM-1 (TCM-9) 524s burn, 100 kg, 316 m/s  
2006 Feb 23  1600 TCM-10 1.4 m/s 2min burn 
2006 Sep 12  2300 TCM-11A 1.7m/s 240s 
 2310  TCM-11B 202s burn 
2006 Oct 5  2230:00  TCM-12 0.5m/s 58s 
2006 Oct 23  0207  Enter Venus sphere 1.008Mkm 
2006 Oct 23  1400?  Enter Venus SOI 
2006 Oct 24 0834  Venus-1 flyby 2990 km altitude 

 

  2986 x -23046 x 116.51  
2006 Oct 25  0300?  Leave Venus SOI 
2006 Oct 25  1503  Depart Venus sphere 1.008Mkm 
2006 Nov 12    224.72d 0.5455 x 0.9013AU x 7.96 
2006 Dec 2  2100  TCM-13a 1670s (Tot TCM-13 is 25.6m/s) 
 2200  TCM-13b 97s 
2006 Dec 3  0300  TCM-13c 1640s 
2007 Apr 25  1730  TCM-15 0.6m/s 
2007 May 25  1600  TCM-16 0.2m/s 
2007 Jun 4  1639  Enter V sphere 1.008Mkm 
2007 Jun 5 2308:19  Venus-2 flyby 338 km (or 313 km)  338 x -20430 x 159.75 

2007 Jun 7  

0540  Depart V sphere 
2007 Oct 17  2200  DSM-2 (TCM-18A), 5min 70 kg 226 m/s  
 2230  DSM-2 (TCM-18B) small correction 
2007 Dec 19  2200  TCM-19 1:51 1.1m/s 
2008 Jan 14  0934  Enter Mercury sphere at 201498 km 
2008 Jan 14  1350  Enter Mercury SOI 
2008 Jan 14 1904:39  Mercury-1 flyby 2640 km C/A  200 x -6388 x 4.99  

2008 Jan 15  

0025  Leave Mercury SOI 
2008 Jan 15  0429  Depart Mercury sphere at 198985 km 
2008 Feb   Solar orbit cruise: 3 M-years, 2 probe orbits 
2008 Mar 19   DSM-3 2.5min 72m/s 21 kg 
2008 Jun 5   Fast earth-rel vel of 90.92 km/s 
2008 Oct 5  2222  Enter M sphere at 196378 km 
2008 Oct 6 0840:20s  Mercury-2 flyby 2640 km C/A  199 x -6722 x 0.85 
2008 Oct 6  1852  Depart M sphere at 193789 km 
2008 Nov   Solar orbit cruise: 4 M-years, 3 probe orbits 
2008 Dec 4 2030 DSM-4a (TCM-29a) 219m/s 4.5min 
2008 Dec 8 2030 DSM-4b 24.7m/s 
2009 May 10    117.68 0.3096 x 0.6304 AU x 6.99 
2009 Sep 29  0741  Enter M sphere at 179899 km  
2009 Sep 29  1310  Enter Mercury sphere  
 2156  M3 flyby 228 km  228 x -8959 x 0.33  
2009 Sep 30  0640  Leave Mercury sphere 
2009 Sep 30  1200  Leave Mercury sphere at 178006 km 
2009 Oct   Solar orbit cruise: 6 M-years, 5 probe orbits 
2009 Nov 24    104.80d 0.3028 x 0.5672 AU x 7.01 
2009 Nov 24 2145:00 DSM-5 (TCM-35) 177.75m/s 
 2149:10  DSM-5 off 
2009 Nov 30    105.71d 0.3079 x 0.5672 AU x 7.03 deg 
2011 Mar 17  0423  Enter M sphere 175230 km 
2011 Mar 18   Mercury-4 approach  269 x -14261 x 79.94  
2011 Mar 18  Mercury-4, orbit insertion  
 0045  MOI-1 (TCM-43) 14 min, 180 kg prop.  
 0100  MOI-1 complete 861.63m/s 
 0647  Apogee 1  
 1248? Perigee 1 
 1848  Apogee 2  
   207 x 15261 x 82.5  
2011 Jun 14    492 x 14882 x 82.9 
2011 Jun 15  1940 OCM-1 Lower periapsis, TCM 15s, 28m/s  200 x 14867 x 83.0  
2011 Jul 26    12.00h 
2011 Jul 26  2104  OCM-2 Tweak apogee 4.1m/s 3.1min 11.80h  
2011 Aug 1    320 x 15066 x 83.2 
2011 Sep 7    12.00h 470 x  
2011 Sep 7  1508  OCM-3 25.0m/s 11.76h 200 x  
2011 Oct 24    11.76h 
 2211  OCM-4 4.2m/s  12.00h  
2011 Dec    12.00h 442 x  
2011 Dec 5  1608  OCM-5 22.2m/s  11.79h 200 x  
2012 Mar   End of main mission  11.79h 405 x  
2012 Mar 3  0144  OCM-6 19.2m/s  11.60h 200 x  
2012 Apr 12   Orbit period 11:36  
2012 Apr 16  1913  OCM-7 Orbit adjust 188s 53.3m/s, oxi deplete 
  Orbit period 9:05 
2012 Apr 20  2305:35 OCM-8 Orbit adjust for extended mission,31.5 m/s 
  Orbit period 8h  278 x 10314 x  
2013 Mar 18   Periapse 450 km 
2013 Dec   Periapse 300 km 
2014 Mar 23   Periapse 200 km? 
2014 Jun 17    114 x  
2014 Jun 17  1453:42  OCM-9 5m/s  155.1 x  
2014 Sep 12  1554  Periapse 25 km, start increase  24.3 x  
2014 Sep 12   OCM-10 8.5 m/s  94 x  
2014 Oct 21  CDM-161 0.004m/s 
2014 Oct 24   Periapse 25 km  
  OCM-11 19.3 m/s 
2014 Oct 28   CDM-162 0.003m/s 
2014 Nov 4   CDM-163 0.003m/s 
2014 Nov 18   CDM-164 0.003m/s 
2014 Dec 24  Peri 101 km  
2015 Jan 21   Periapse 25 km 
  OCM-12 9.7m/s to 80 km  
2015 Mar 1   Periapse 15 km 
2015 Mar 18    496.5 11.6 x 10932 x 83.1  
2015 Mar 18  1500  OCM-13 33s 3.1m/s  497.6 34.5 x 10933 x 83.1  
2015 Apr 2   497.6 5.5 x 10949 x 83.5  
2015 Apr 2  2029:46 OCM-14 6.3min 3.11m/s  498.8 28.3 x 10942 x 83.4  
2015 Apr 6    498.9 13.1 x 10980 x 83.4  
2015 Apr 6  1614:06 OCM-15 6.3min 1.77m/s  499.4 25.7 x 10989 x 83.4 
2015 Apr 8  1655:15 OCM-15A 5m 1.94m/s He pressurant mvr  500.3 29.1 x 10997 x 83.3  
2015 Apr 14   6.5 x 11015 x 83.1  
2015 Apr 14  1516  OCM-16 0.98m/s  500.7 12 x 11018 x 83.0  
2015 Apr 28  0038  Periapse R = 2449 km h=9 km 
2015 Apr 30  1108  Periapse h = 0 km  0 x 11001 x 83.3  
2015 Apr 30  1926:02 Impact 54.4N 210.1E at 3.91 km/s  -3 x 11003 x 83.3  

Payload:

  • 667N Leros-1b (Ampac-ISP)

  • 4 x 22N Aerojet MR-106E mono hydrazine thrusters, small burns.

  • 12 x 4N Aerojet MR-111C thrusters

  • MDIS Mercury Dual Imaging System;

    • Wide angle CCD imager, 10.5 deg FOV, 0.4-1.1 mu, 12 filters

    • Narrow angle CCD imager 1.5 deg FOV, 18m res, monochromatic

  • GNRS Gamma ray and neutron spectrometer, with cryocooler

  • XRS X-ray spectrometer, collimated gas counters, 1-10 keV

  • MAG Magnetometer, 3-axis ring-core fluxgate, 50-ms time resolution.

  • MLA Mercury Laser Altimeter, 30cm res, 1.06mu

  • MASCS Mercury Atmospheric and Surface Composition Spectrometer, UV/Vis spectrometer and Vis/IR spectrograph.

  • EPPS Energetic Particle and Plasma Spectrometer, with energetic particle spectrometer (EPS) and fast imaging plasma spectrometer (FIPS) for composition, energy and pitch angle for ions and electrons

Ekspress 3

 2000-013A


Intersputnik's Ekspress A2 will be stationed at the 80E Ekspress 6A location. The satellite was built for Gos. pred. Kosmicheskaya Svyaz (GPKS)lthe Intersputnik operator.

The second Ekspress A Russian communications satellite was successfully launched on Mar 12 by a Krunichev Proton-K from Baykonur. Ekspress A No. 2 will be assigned to the Ekspress 6A slot at 80E, providing communications for GO Kosmicheskaya Svyaz. The Ekspress A is built by NPO PM, with a communications payload from Alcatel. The spacecraft is also known as Ekspress 14.

Launch mass was 2600 kg.


Ekspress A2 
 

DateTimeEventOrbit  

2000 Mar 12  0407:00  Launch by Proton/DM  KB 
 0416  Stage 3 MECO 
 0416  Stage 3 sep  195 x 227 x 51.6 
 0417? Upper adapter sep 
 0524? Transfer orbit perigee 
 0524?  DM 2M No 10L MES-1 
  MECO-1  222 x 35702 x 48.7 
 1038?  DM MES-2 
 1038? DM MECO-2 
 1039:48  DM sep 
2000 Mar 13    1432.43 35687 x 35741 x 0.2 GEO 92.2E+0.9E 
2000 Mar 21    1436.10 35779 x 35794 x 0.2 GEO 96.6E 
2000 Apr 17    1436.17 35780 x 35795 x 0.1 GEO 96.4E 
2000 Apr 27    1436.12 35771 x 35802 x 0.1 GEO 96.5E 
2000 Apr 30   mv out 
2000 May 11    1439.03 35816 x 35871 x 0.1 GEO 80.1E+0.7E 
2000 May 26    1436.11 35778 x 35795 x 0.1 GEO 80.2E 
2003 Nov 6    1436.10 35770 x 35802 x 0.0 GEO 80.0E 
2005 Oct 17    1436.13 35777 x 35796 x 0.1 GEO 80.1E 
2005 Oct 17   Move out 
2005 Nov 7  Move in at 103.0E 
2006 Aug 3   1436.12 35778 x 35796 x 0.6 GEO 103.0E 
2014 Jun 24    1436.13 35628 x 35945 x 7.2 GEO 103.1E 
2014 Jun 28   Move out 
2014 Aug 29   Move in at 145E 
2014 Aug 29    1436.10 35723 x 35850 x 7.4 GEO 145.2E 
2015 Oct 26    1436.12 35698 x 35875 x 8.1 GEO 144.9E 

Sunday, December 20, 2015

Globalstar 19

 1999-019A



Globalstar M019 
 

DateTimeEventOrbit  

1999 Apr 15  0046  Launch by Soyuz-U/Ikar 
  T+1:58 Blok BVGD sep 
  T+2:38 Fairing sep 
  T+4:43 Blok A sep 
 0055  T+8:48 Blok I sep 
 0315  T+2:29:31 Ikar burn 
 0419  T+3:33:30 M19 sep 
1999 Apr 20    103.50 903 x 944 x 51.9 
1999 Jul 8   Burns begin 103.51 905 x 944 x 51.9 
1999 Aug 5    106.06 1019 x 1068 x 52.0 
1999 Aug 14    111.06 1260 x 1290 x 52.0 
1999 Sep 9    112.63 1342 x 1351 x 52.0 
1999 Sep 19    114.06 1411 x 1413 x 52.0 
1999 Sep 30    114.08 1412 x 1414 x 52.0 
2013 Jun 16    114.08 1413 x 1413 x 52.0 

November 20,2006

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