Saturday, February 28, 2004

Kosmos 2367

 1999-072A


A few weeks after the reentry of Kosmos-2347, Kosmos-2367 was launched to replace it, again the only satellite in the system. The satellite was a US-PU or US-PM variant.

RCS was 22m2. Only 13 debris objects were tracked, apparently all small.


Kosmos-2367 
 

DateTimeEventOrbit  

1999 Dec 26  0800 Launch by 11K69 No 801  KB LC90 
  T+2:01 St 1 sep 
  T+4:07 Fairing 
  T+4:39 SECO, 
 0804  T+4:39 St 2 sep 147 x 442 x 65.0 
 0848  T+48:04 DU burn 
 0848  T+48:32 DUCO 
1999 Dec 26    404 x 417 x 65.0 
2001 Nov 21  1410? Debris event, out of service 
2002 Jul 20  0004?  Reentered over S Pacific 

Friday, February 20, 2004

Kosmos 2365

 1999-044A



Kosmos-2365 
 

DateTimeEventOrbit  

1999 Aug 18  1800  Launch by Soyuz-U  PL 43/3 
 1804?  Blok A sep 
 1808?  Blok I MECO 
 1808?  Blok I sep 
   89.60 166 x 342 x 67.1 
1999 Aug 19    89.56 166 x 339 x 67.1 
1999 Aug 25    88.98 158 x 289 x 67.1 
1999 Aug 25   Orbit raise  89.96 175 x 369 x 67.1 
1999 Sep 1    89.43 169 x 323 x 67.1 
1999 Sep 1   Orbit raise  90.06 184 x 370 x 67.1 
1999 Sep 15    89.35 175 x 309 x 67.1 
1999 Sep 16   Orbit raise  89.80 185 x 343 x 67.1 
1999 Sep 23    89.38 179 x 308 x 67.1 
1999 Sep 24   Orbit raise  89.94 188 x 354 x 67.1 
1999 Oct 6    89.16 175 x 290 x 67.1 
  Orbit raise 90.11 195 x 364 x 67.1 
1999 Oct 70105? SpK deorbit fiducial 
 0116? Reentry 
 0128? SpK recovered 
1999 Oct 8 
89.98 190 x 356 x 67.1 
1999 Oct 9    89.92 188 x 352 x 67.1 
1999 Oct 20    89.18 176 x 291 x 67.1 
1999 Oct 24    88.64 163 x 250 x 67.1 
1999 Oct 24   Orbit raise 90.00 181 x 366 x 67.1 
1999 Oct 27    89.86 180 x 354 x 67.1 
1999 Oct 27   Orbit raise 90.56 193 x 410 x 67.1 
1999 Nov 15  1228? SpK-2 fiducial 
 1238? Reentry 
 1250? Landed 
1999 Nov 17    89.42 174 x 316 x 67.1 
1999 Nov 17   Orbit raise 89.73 185 x 336 x 67.1 
1999 Nov 23    89.30 176 x 302 x 67.1 
1999 Nov 23   Orbit raise 90.20 179 x 389 x 67.1 
1999 Dec 2    89.89 183 x 355 x 67.1 
1999 Dec 5    89.57 180 x 326 x 67.1 
1999 Dec 14    88.76 166 x 259 x 67.1 
1999 Dec 14   Orbit raise 89.23 190 x 282 x 67.1 
1999 Dec 15    89.20 190 x 280 x 67.1 
1999 Dec 16  Orbit lower 88.34 165 x 219 x 67.1 
 1100 88.27 163 x 214 x 67.1 
 1250?  Deorbit  -183? x 163 x 67.1 
 1304?  Reentry 
 1316?  Landed 

JCSAT 3

 1995-043A


The third JCSAT satellite was an HS-601 model rather than the older spinning satellites used for JCSAT 1 and 2. It was launched on an Atlas 2AS, flight 8205/AC-117, on 1995 Aug 29. JCSAT 3 is owned by Japan Satellite Systems (JSS).

It is the first Japanese digital TV broadcasting satellite, and will be operated by DMC (Digital Multi-Channel Planning Co, Ltd), a partnership of JSAT (Japan Satellite Corp), Itochu Corp, Mitsui and Co, Ltd, Nissho Iwai Corp and Sumitomo Corp. The satellite will also provide data and fax transmission services.

JCSAT 3 was launched into a supersynchronous transfer orbit with an apogee of 80000 km. Space Command's circa-250-km initial perigee is a tracking error; the initial perigee was 167 km, a difference of 5m/s at apogee.


JCSAT 3 
 

DateTimeEventOrbit  

1995 Aug 29  0053:01  Launch by Atlas IIAS (AC-117)  CC LC36 
  Atlas 8205 sep 
 0058:17 Centaur AC-117 MES1 (4:26) 
 0102:44 Centaur AC-117 MECO1, parking orbit 155 x 395 x 28.2 
 0116:45 Centaur AC-117 MES2 (1:47) 
 0118:32 Centaur AC-117 MECO2, transfer orbit  
 0120? Centaur AC-117 sep  260 x 80799 x 23.2  
   1681.65 248 x 80682 x 23.1 (TLE) 
   1681.65 167 x 80684 x 23.1 (Est) 
1995 Aug 30    1685.13 260 x 80799 x 23.2 
 1924  First apogee on equator at 99W 
1995 Sep 31050?LAM-1 
1995 Sep 82100?LAM-2 
1995 Sep 10    1621.15 35718 x 42951 x 0.25 
1995 Sep 12  1430?  LAM-3 
1995 Sep 14    1437.46 35704 x 35921 x 0.1 GEO 128.2E+0.3E 
1995 Oct 2    1436.03 35740 x 35830 x 0.0 GEO 127.5E 
1995 Dec 30    1436.14 35782 x 35792 x 0.0 GEO 128.0E 
1997 May 25    1436.16 35782 x 35793 x 0.0 GEO 128.0E 
2002 Mar 6  1436.14 35779 x 35795 x 0.0 GEO 128.0E 

The Rocket Men : Vostok and Voskhod, the First Soviet Manned Spaceflights

 https://welib.org/md5/bda7653c8720c9a1136bb73fcd077938

Wednesday, February 18, 2004

Telecom 2A

 1991-084A


France Telecom's Telecom 2 series used the Matra/BAe Eurostar 2000 bus. The 2200 kg satellite carried 10 C-band transponders for communications with the Departements et Terretoires d'outremer (the overseas parts of the French Republic), 11 Ku-band transponders for business communications, and 5 X-band transponders for the Syracuse military system. By 1995 Telecom 2A was mostly dedicated to military communications.


Telecom 2A 
 

DateTimeEventOrbit  

1991 Dec 16  2319:48  Launch by Ariane (V48)  CSG ELA2 
  T+2:27 PAL sep 
  T+3:32 St 1 sep 
  T+3:35 St 2 MES 
  T+4:05 Fairing 
  T+5:43 St 2 sep 
  T+5:48 St 3 MES 
 2337:38 T+17:50 St 3 MECO 
 2339:54  T+20:06 Telecom 2A sep 
 2342:12 T+22:24 Spelda sep 
 2344:21 T+24:33 Inmarsat 2F3 sep 
   645.25 362 x 36351 x 3.8 
1991 Dec 18? 1100? LAM-1 
1991 Dec 18    765.50 6938 x 35744 x 1.9  
1991 Dec 20  1530? LAM-2 1333.19 31732 x 35762 x 0.1  
1991 Dec 22    1332.24 31692 x 35764 x 0.1 
1991 Dec 23  1000? LAM-3 
1991 Dec 24    1433.38 35708 x 35758 x 0.2 GEO 3.7E+0.7E 
1992 Jan 12   mv in  1436.16 35776 x 35798 x 0.1 GEO 3.1E 
1992 Jan 30    1436.07 35771 x 35801 x 0.0 GEO 3.0E 
1992 Feb 28    1436.04 35770 x 35800 x 0.0 GEO 3.1E 
1992 Mar   mv to 8W 
1992 Apr 5    1436.07 35780 x 35791 x 0.0 GEO 8.0W 
1992 Jun 8    1436.11 35782 x 35791 x 0.1 GEO 8.0W 
1995 Oct 14    1436.08 35764 x 35808 x 0.0 GEO 8.0W 
1998 Oct 22    1436.08 35768 x 35803 x 0.0 GEO 8.0W 
1999 Jun 16    1436.10 35766 x 35807 x 0.0 GEO 8.0W 
1999 Jul   Control to Eutelsat 
2001 Oct 23    1436.10 35765 x 35807 x 0.3 GEO 8.1W 
2001 Oct 25   Mv out from 9W 
2001 Nov 14   Mv in 3E 
2001 Nov 28    1436.08 35767 x 35805 x 0.4 GEO 3.0E 
2003 Sep 2    1436.09 35762 x 35809 x 2.0 GEO 3.0E 

Sunday, February 8, 2004

Palapa B2(R)

 1984-011D


After the failure of Westar 6, Palapa B2 was deployed from Challenger's payload bay. The PAM-D ignited, and again the nozzle failed, stranding the satellite in an elliptical orbit. The recovered satellite was bought by Sattel Technologies, Inc. and refurbished, then relaunched for Perumtel as Palapa B2R.


Palapa B2 
 

DateTimeEventOrbit  

1984 Feb 6  1513:16  Palapa B2 deploy from OV-099 
 1558  PAM-D burn 
  Star 37 nozzle fails  
 1559?  PAM-D sep 
1984 Feb 6    99.43 276 x 1186 x 28.2 
1984 Feb 8    99.42 276 x 1185 x 28.2 
1984 Feb 9    99.32 267 x 1185 x 28.2 
1984 Feb 23    99.26 266 x 1179 x 28.2 
1984 Apr 26    98.83 265 x 1139 x 28.2 
1984 May 16    98.89 271 x 1139 x 28.2 
1984 May 16  1408 Star 30B burn  109.89 1134 x 1308 x 28.5 
1984 Jul 22    109.89 1133 x 1309 x 28.5 
1984 Aug 6   Lower orbit  106.09 1028 x 1062 x 28.5 
1984 Oct 9    106.09 1028 x 1062 x 28.5 
1984 Oct 9   mv  106.16 1026 x 1070 x 28.5 
1984 Oct 11   Lower orbit  105.36 954 x 1067 x 28.5 
1984 Oct 12   Lower orbit  102.74 708 x 1067 x 28.5 
1984 Oct 13   Lower orbit  100.49 493 x 1070 x 28.5 
1984 Oct 14   Lower orbit  99.20 365 x 1075 x 28.5 
1984 Oct 15   Lower orbit  99.20 365 x 1074 x 28.5 
1984 Oct 16   Lower orbit  99.02 357 x 1065 x 28.5 
1984 Oct 18   Lower orbit  97.96 357 x 964 x 28.5 
1984 Oct 20   Lower orbit  96.99 358 x 870 x 28.5 
1984 Oct 23   Lower orbit  95.05 360 x 681 x 28.5 
1984 Oct 25   Lower orbit  93.24 361 x 504 x 28.5 
1984 Oct 26   Lower orbit  93.10 362 x 489 x 28.5 
1984 Oct 28   Lower orbit  92.69 362 x 450 x 28.5 
1984 Oct 30   Lower orbit  91.80 357 x 368 x 28.5 
1984 Oct 31   mv  91.86 351 x 379 x 28.5 
1984 Nov 1   mv  91.83 353 x 374 x 28.5 
1984 Nov 2   mv  91.90 358 x 376 x 28.5 
1984 Nov 4    91.82 355 x 371 x 28.5 
1984 Nov 12    91.78 353 x 370 x 28.5 
1984 Nov 12   OV-103 rendezvous Palapa B2 
 1443  MMU/Allen dock Palapa  
 1453  RMS grapple Palapa 
 1610?  MMU-3 undock ACD 
 1713  Palapa B2 berthed 
1990   Renamed Palapa B2R 
1990 Apr 13  2228:00 Launch by Delta 6925-8 CC LC17B 
  95 deg azimuth 
  T+1:03 SRM off 
  T+2:09 SRM off 
  T+4:20 MECO 
  T+4:37 SES-1 
 2232  T+4:38 Fairing 
 2239?  T+11? SECO-1  180? x 500? x 28? 
 2245? T+17? SES-2? 
 2245? SECO-2?  500? x 1400? x 25?  
 2245? St 2 sep 
 2246? T+18? TES 1:27 
 2247? TECO 
 2254? PAM-D sep  674.96 445 x 37775 x 18.0 
 2336? Delta depletion  104.20 495 x 1418 x 22.8 
1990 Apr 15    674.97 445 x 37776 x 18.0 
1990 Apr 16  0120? AKM 
1990 Apr 16    1485.63 35716 x 37784 x 0.4 GEO 134.9E+12.0W 
1990 Apr 17  1100? mv in  
1990 Apr 17    1436.07 35669 x 35902 x 0.1 GEO 117.8E 
1990 Apr 17   Solar panels deployed 
1990 May 1    1436.04 35660 x 35910 x 0.1 GEO 118.1E 
1990 May 11   mv out 
1990 May 17    1438.53 35785 x 35883 x 0.0 GEO 114.6E+0.6W 
1990 Jun 4   mv in  1436.08 35782 x 35790 x 0.0 GEO 107.9E 
1992 Jul 31    1436.15 35785 x 35790 x 0.0 GEO 108.0E 
1994 Mar 6    1436.16 35784 x 35791 x 0.0 GEO 108.0E 
1996 Jun 19    1436.11 35784 x 35788 x 0.0 GEO 108.1E 
1999 Jun 14    1436.11 35786 x 35787 x 0.1 GEO 108.1E 
2000 Dec 19    1436.22 35787 x 35790 x 0.5 GEO 108.2E 
2001 Jan 2   mv out  1445.91 35810 x 36146 x 0.6  
2001 Jan 19   mv in  1436.09 35783 x 35789 x 0.6 GEO 42.5E 
2001 Apr?   Renamed Newsat-1 
  Bought by Newsat USA, NJ and Bermuda 
2001 Oct 8    1436.05 35736 x 35834 x 1.2 GEO 42.6E 
2003 Jul 2    1436.04 35782 x 35788 x 2.8 GEO 42.5E 

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