Friday, April 16, 2004

Meteosat 5

 1991-015B


The second EUMETSAT MOP satellite, MOP 2/Meteosat 5, was launched in Mar 1991. On 1995 Dec 1, EUMETSAT took control of the spacecraft at its Darmstadt mission control center, taking over from the European Space Agency's ESOC site. In Jan 1998 Meteosat-5 was replaced by Meteosat 7 and began drifting to the Indian Ocean to participate in the Indoex program at 67E, studying cloud formation and atmospheric pollution in an international experiment.


Meteosat 5 (MOP 2) 
 

DateTimeEventOrbit  

1991 Mar 2  2336:00  Launch by Ariane 44LP  CSG ELA2 
  T+1:06 PAP sep 
  T+2:29 PAL sep 
  T+3:32 St 1 sep 
  T+3:35 St 2 MES 
 2340 T+4:33 Fairing sep 
 2341 T+5:43 St 2 sep 
 2341 T+5:46 St 3 MES 
 2353:47 T+17:47 St 3 MECO  640.93 240 x 36252 x 7.1 
 2356:11 T+20:11 Astra 1B sep 
 2358:39 T+22:39 Spelda sep 
1991 Mar 3  0000:35 T+24:35 MOP 2 sep 
1991 Mar 3  0021:00  T+45m spinup, 40 kg fuel; 682 kg total 
 0250:00  Sun angle correction 
 0345  Attitude slew 1 
 1210  Attitude slew 2 
 1434:14  Attitude slew 3 
1991 Mar 4    632.57 194 x 35869 x 7.05 
1991 Mar 4  1334:12  MAGE 1 burn 
 1339 MAGE 1 eject
 1410Spin axis erection; mass 322.1 kg 
1991 Mar 4    1424.84 35146 x 35985 x 1.2 GEO 32.1W+2.8E 
1991 Mar 5  0105:42  Drift correction 4.9m/s
1991 Mar 5  1200  Control to payload commissioning  1431.52 35413 x 35980 x 1.20 GEO 29.5W-1.1/d 
1991 Mar 7  1000   1431.65 35413 x 35985 x 1.20 GEO 27.9W-1.1/d 
1991 Mar 23    1435.66 35767 x 35788 x 1.2 GEO 4.3W 
1991 Mar 29    1435.79 35770 x 35791 x 1.2 GEO 3.9W 
1991 Apr   mv to 1W 
1991 Apr 3   Radiometer baffle cover ejected 
  Radiometer cooler cover ejected 
 1125  First image 
1991 May 1    1435.72 35771 x 35786 x 1.1 GEO 1.0W 
1991 May 24   moving to 4W 
1991 Jun 4    1436.53 35784 x 35805 x 1.0 GEO 3.9W 
1991 Oct 22    1436.08 35777 x 35795 x 0.8 GEO 4.0W 
1992 Jan 14   Ownership to EUMETSAT 
1992 Jul 12    1436.04 35777 x 35793 x 0.6 GEO 3.9W 
1992 Aug 3    1435.87 35778x 35786 x 0.2 GEO 3.6W+0.05E 
1992 Aug   Move to 1W 
1992 Sep 7    1435.75 35771 x 35788 x 0.2 GEO 0.8W 
1992 Nov 6    1436.45 35786 x 35800 x 0.1 GEO 0.8W 
1992 Nov   Move out, drift to 8W? 
1992 Nov 20    1436.33 35782 x 35799 x 0.1 GEO 3.6W+0.06W 
1993 Feb 9    1436.23 35782 x 35796 x 0.2 GEO 6.7W+0.04W 
1993 Jun 29    1436.19 35785 x 35791 x 0.2 GEO 7.3W+0.03W 
1993 Sep 3    1436.10 35781 x 35792 x 0.2 GEO 7.8W 
1993 Sep 24    1436.09 35781 x 35791 x 0.2 GEO 7.7W 
1993 Oct   Move to 0E 
1993 Oct 29    1436.02 35757 x 35812 x 0.3 GEO 0.5E 
1993 Nov 18    1436.22 35784 x 35793 x 0.3 GEO 0.3W 
1994 Apr 5    1436.05 35779 x 35792 x 0.2 GEO 1.2W 
1994 Jul 24    1436.12 35779 x 35794 x 0.3 GEO 0.1E 
1995 Jan 28    1436.24 35783 x 35794 x 0.1 GEO 1.0W 
1995 Dec 1   Control to EUMETSAT-Darmstadt 
1996 Apr 14    1436.19 35781 x 35795 x 0.4 GEO 0.2E 
1997 Mar 13    1436.84 35789 x 35814 x 1.1 GEO 1.6E 
1997 Mar 15   GEO mv out  GEO 0E 
1997 May 18   mv in  
1997 May 22    1436.07 35782 x 35780 x 1.2 GEO 9.7W 
1998 Jan 13    1436.07 35768 x 35803 x 1.7 GEO 9.2W 
1998 Jan 18   mv out  
1998 May 19   mv in  GEO  
1998 Jun 23    1436.00 35756 x 35812 x 2.0 GEO 63.4E 
1998 Jul 1   Start Indoex data 
1998 Nov 30    1435.98 35779 x 35789 x 2.3 GEO 63.3E 
1999 Jun 15    1436.04 35758 x 35812 x 2.8 GEO 62.5E 
2003 Aug 26    1436.11 35779 x 35793 x 6.1 GEO 62.8E 

Team of the century : the greatest high school football team in Texas

 https://welib.org/md5/0d7e28457242beb17f119a4144b700a6

Sunday, April 11, 2004

Kosmos 613

  1973-096A


7K-T 11F615A8 No. 34A was the third test flight of the stripped-down Soyuz ferry. It flew a 60 day long duration test to confirm that the systems would survive an extended stay powered down while docked to a DOS or Almaz station. The orbital module was jettisoned prior to retrofire and remained in orbit until 1974 Mar 9.


Kosmos-613 
 

DateTimeEventOrbit  

1973 Nov 30  0520  Launch by Soyuz 11A511  KB
 0524  Blok-I burn 
 0529  Blok-I sep  
 1430  89.04 187 x 268 x 51.61 
1973 Dec 1  0230  89.11 188 x 273 x 51.60 
1973 Dec 3    88.97 185 x 263 x 51.60 
  Orbit raise 
1973 Dec 3  0930   89.26 200 x 277 x 51.6 
1973 Dec 5    89.10 201 x 259 x 51.6 
 1200? Orbit raise  91.06 253 x 400 x 51.62 
1974 Jan 11    90.78 250 x 377 x 51.59 
1974 Jan 28  0930   90.58 239 x 366 x 51.59 
1974 Jan 29 
 0340? Orbital module sep 96C 
 0458? Rev 953/TLE24: Node 2E good opp 
 0449? Retrofire 
 0452? DO CO 
 0507? PAO sep? 
 0513? Entry 
 0536? Landed after 60.1d 

Saturn S-IVB-507

  1969-099B


SA-507 was launched on 1969 Nov 14 at 1622. The TLI burn was at 1909, and Apollo 12 separated at 2035. The propellants were dumped and the stage flew past the Moon at 5724 km on 1969 Nov 18 at 0610. A trajectory error left S-IVB-507 in a 165000 x 850000 km Earth orbit instead of the intended solar orbit.

The closest apporach of 5715 km above the lunar surface was not close enough to accelerate the stage to escape; an inaccurate state vector meant that the commanded ullage burn was too long. The flyby increased the geocentric speed of the stage by 0.548 km/s.


S-4B-507 
 

DateTimeEventOrbit  

1969 Nov 14  1622:00  Range zero 
 1622:00  Launch by Saturn V (SA-507)  KSC LC39A 
 1622:36  Lightning strike on SA-507, 1.95 km alt 
 1622:52  Second small lightning strike 
 1624:15  S-IC CECO 
 1624:42  S-IC OECO, sep  -6009 x 123 x 32.1  
 1624:44  S-II ignition 
 1625:12  Interstage 
 1625:18  LES jett 
 1629:41  S-II CECO 
 1631:12  S-II OECO 
 1631:13  S-II sep  -2011 x 191 x 32.70  
 1631:14  T+9:14 SIC impact 30.27N 73.90W 
 1631:16  S-IVB ignition 
 1631:25  Ullage case sep 
 1631:41  T+9:41 S-II apogee  
 1633:34  S-IVB shutdown 
 1633:44  Earth orbit insertion  88.2 181 x 185 x 32.54  
 1642:21  T+20:21 S-II impact 31.47N 34.21W  
 1909:25  S-IVB TLI burn 
 1915:04  S-IVB cutoff 
 1915:14  Translunar injection  215 x 409386 x 30.360 
   215 x 409138 x 30.36 
   215 x 428571 x 30.36 
V tab 4.6    215 x 428200 x 30.36 
C3 tab 4.6  1940:05  Sep from S-IVB/SLA  219 x 424147 x 30.42  
  Transposition and docking maneuver 
 1948:53  Docked with LM/S-IVB 
 2035:01  CSM/LM sep from S-IVB 
 2048:40  APS evasive 2.9m/s 
 2058:20  CVS LH2 vent 2.8m/s 
 2110:00  LOX dump 10.0 
 2110:58  LOX dump end 
 2112:07  LH2 NPV 
  APS-1 11.8m/s 300s 
  APS-2 10.7m/s 270s 
 2150:20  APS burn end 
1969 Nov 17  1344  Enter lunar sphere 66183 km 
1969 Nov 18  0610 Lunar flyby  5709 x -19546 x 20.43 
  Trailing edge, 7000 km  
1969 Nov 18 2236  Depart lunar sphere 66183 km 
1969 Dec    150000-176000 x 830000-890000  
1969 Dec    165000 x 850000  
1971 Mar?   Escape via L1 
2002 Apr   Capture via L1 
2002   Detected as J002E3 
2002 Jun 12 1358 TDB 160967 km from Moon 
2002 Jun 15 1957  193878 km perigee 
2002 Aug 9  0752  238608 km from Moon 
2002 Aug 11 0250  365916 km perigee 
2002 Aug 21  2119  252222 km from Moon 
2002 Sep 28  1402  232175 km perigee 
2002 Dec 16   144062 km perigee 
2003 Jun 19  0100 Depart Earth sphere via L1 

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt