Saturday, June 12, 1999

Mars 1C

  1962-057A


Shortly after the Venus window closed, the 1962 Mars window opened and 2MV-4 No. 1 was launched, an intended Mars flyby probe. The Blok-L fourth stage on this mission exploded 16s into its burn when a turbopump jammed. A number of debris fragments were tracked by the US, causing some momentary alarm during this Cuban missile crisis period. Again, the launch was not announced by the USSR. It is not clear which of the objects tracked was the rocket body or the BOZ motor. The longest lived objects were BetaIota 3, decayed 1963 Feb 26, and BetaIota 8, decayed Jan 2.

The date of the event is recorded as Oct 29 in Johnson's fragmentation catalog, but that's just the recorded decay date of object 1962 BetaIota 1; it is clear from Russian sources that the explosion was actually on Oct 24.


2MV-4 No. 1 
 

DateTimeEventOrbit  

1962 Oct 24  1755:04  Launch by 8K78  KB 
 1800  Blok-A sep 
 1800  Blok-I burn 
 1804  Blok-I sep  180 x 485 x 64.9 
 1855?  BOZ burn 
 1856?  Blok-L burn 
 1856?  Blok-L exploded   

Gorizont 4

 1980-049A


The fourth Gorizont satellite (Gorizont No. 15L) was launched in Jun 1980 to the Atlantic (Statsionar 4) location. 


Gorizont 15L
 

DateTimeEventOrbit  

1980 Jun 14  0049:50 Launch by Proton  KB 
 0059 Stage 3 sep 
 0207? DM burn 1  632.20 314 x 35730 x 47.5 
 0723? DM burn 2 
 0727? Blok-DM No. 27L sep 
   1472.95 36290 x 36719 x 0.8 GEO 90.5E+9.0W 
1980 Jun 23    1473.19 36380 x 36638 x 0.8 GEO 7.8E+9.1W 
1980 Jun 27    1436.05 35744 x 35827 x 0.8 GEO 14.5W 
1980 Oct 2    1436.09 35737 x 35835 x 0.6 GEO 13.6W 
1981 Jan 21    1436.18 35746 x 35829 x 0.4 GEO 14.6W 
1981 Jun   Statsionar 4 location  GEO 14W 
1982 Jan 1    1436.15 35748 x 35827 x 0.4 GEO 14.1W 
1983 Jan 2    1436.14 35747 x 35826 x 1.2 GEO 13.9W 
1984 Jan 4    1436.09 35755 x 35817 x 2.1 GEO 13.7W 
1984 May 2    1436.10 35771 x 35801 x 2.4 GEO 13.6W 
1984 May   Move to 11.2W 
1984 May 13    1436.06 35775 x 35796 x 2.5 GEO 11.2W 
1984 Jul 14    1436.06 35765 x 35806 x 2.6 GEO 10.8W 
1985 Jan 23    1436.10 35769 x 35804 x 3.1 GEO 10.8W 
1985 Apr 25    1436.09 35779 x 35793 x 3.3 GEO 10.8W 
1985 Apr   Move to 13.5W 
1985 May 2    1436.09 35754 x 35818 x 3.3 GEO 13.6W 
1985 Aug 16    1436.09 35758 x 35814 x 3.6 GEO 12.9W 
1985 Aug 23   Move to 11W 
1985 Sep 6    1436.06 35756 x 35815 x 3.6 GEO 11.0W 
1987 Mar 31    1436.12 35750 x 35823 x 5.1 GEO 11.5W 
1988 Oct 20    1436.09 35765 x 35808 x 6.5 GEO 11.0W 
1988 Oct 25   Decommissioned 
1988 Nov 16    1436.18 35764 x 35812 x 6.6 GEO 11.6W+0.03W 
1988 Nov 30   Orbit raise  1460.04 36230 x 36278 x 6.6 GEO 118.3E 
1991 Sep 25    1460.00 36244 x 36261 x 9.2 

Thursday, June 10, 1999

DSCS 9431/9432

 1971-095A


Satellite 9431, the first DSCS II satellite, had a mass of 526 kg after launch. It was probably designated satellite A-1. The satellite's communications system failed in June 1973 due to an electrostatic discharge caused by charging in a substorm. This event raised awareness of the dangers of spacecraft charging in high orbit.


DSCS II A-1 
 

DateTimeEventOrbit  

1971 Nov 3  0309:06  Launch by Titan 3C  CC  
  T+1:49 Stage 1 ignition 
  T+2:02 SRM sep 
  T+4:18 Stage 1 MECO, sep  
 0314 T+5:00? Fairing sep
  T+7:40? SECO 
 0316 T+7:45? Stage 2 sep  145? x 400? x 28.6  
 0419? Transtage burn 1  320? x 37000? x 26.5? 
 0920? Transtage burn 2 
 0930? Transtage sep 
1971 Nov   Operational  GEO POR 
1971 Dec 10  1813   1436.19 35783 x 35792 x 2.6 GEO 106.1W+0.0 
1972 Feb 5    1435.89 35774 x 35791 x 2.4 GEO 111.1W+0.05W 
1973 Jun 2   Charging event, comms failed 
1973 Jun   end of ops 
1975? Moved to 81W 
1977 Feb 25    1435.89 35743 x 35821 x 1.9 GEO 81.6W+0.04W 
1978 Oct 22    1436.19 35761 x 35815 x 3.1 GEO 81.2W+0.0 
1979 Mar 1    1435.70 35749 x 35808 x 3.3 GEO 86.3W 
1979   Moved to 110W 
1979 Aug 27    1436.18 35761 x 35815 x 3.7 GEO 111.0W 
1979 Sep   Drifting GEO 110W 
1980 Jan    GEO 110W 
1980 Oct    GEO 101W 
1980 Mar 1    1435.97 35753 x 35814 x 4.0 GEO 109.7W 
1980 Jun 27    1435.91 35777 x 35789 x 4.3 GEO 104.6W+0.04 
1981    GEO 99-102W 
1982    GEO 109-111W 
1986    GEO 106W 
1988 Jun 5    1436.03 35766 x 35804 x 10.0 GEO 99.2W 
1989 Jan 16    1436.25 35776 x 35803 x 10.5 GEO 102.6W 
1990 Jan 31    1435.98 35768 x 35800 x 11.3 GEO 110.5W 
1992 Jan 31    1436.20 35764 x 35812 x 12.7 GEO 110.5W 
1994 Jan 31    1436.25 35758 x 35821 x 13.8 GEO 102.9W 
1998 Aug 5    1436.05 35753 x 35818 x 15.1 GEO 98.8W 

Payload:

  • X-band transponders

  • Earth coverage antennae; horn antenna

  • 2 narrow coverage parabolic antennae




1971-095B

Satellite 9432, the second of the first DSCS II pair, suffered an accidental spinup of its communications payload platform in Dec 1971, possibly due to spacecraft charging problems, but the satellite was successfully despun in 1972 Jun. Mass of F-2 was 526 kg.


DSCS II A-2 
 

DateTimeEventOrbit  

1971 Nov 3   Launch by Titan 3C  CK 
  Colocated DSCS F-1 GEO POR 
1971 Dec 12  0901   1435.81 35773 x 35788 x 2.6 GEO 115.6W+0.06W/d 
Dec?  Accidental spinup 
1972 Jan 9    1435.43 35568 x 35978 x 2.5 GEO 112.0W+0.1W 
1972 Feb 1    1435.53 35762 x 35788 x 2.4 GEO 89.6W+0.1W 
1972 Jun   Payload despun 
1977 Jan 31    1436.67 35750 x 35845 x 1.7 GEO 140.1E+0.1E 
1978 Feb 6    1437.02 35766 x 35842 x 2.5 GEO 15.5E+0.2E 
1979 Sep 18    1437.78 35780 x 35858x 3.6 GEO 114.1W+0.4E 
1980 May   On station  GEO 175E 
1980 Jul 6    1436.32 35773 x 35808 x 4.1 GEO 176.5E+0.0 
1980 late   Begin slow period decrease 
1980 Dec 13    1435.81 35773 x 35789 x 4.5 GEO 177.6E+0.06 
1981 Jan 5    1435.71 35770 x 35787 x 4.5 GEO 179.5E+0.09 
1981 Jan 31    1435.61 35739 x 35814 x 4.5 GEO 177.7W+0.11W 
1981 May 7    1435.08 35757 x 35776 x 4.7 GEO 160.0W+0.24W 
1981 Jul 25    1434.59 35739 x 35775 x 4.9 GEO 134.5W+0.37W 
1982 Sep 27    1435.65 35748 x 35807 x 5.7 GEO 14.1W+0.2W 
1984 Nov 9    1436.21 35782 x 35796 x 7.2 GEO 149.2E+0.04E 
1985 Feb 1    1436.55 35786 x 35804 x 7.4 GEO 141.3E+0.14E 
1988 Nov 8    1436.06 35772 x 35799 x 10.2 GEO 173.3E+0.00E 
1989 Sep 14    1434.59 35737 x 35776 x 10.9 GEO 135.1W+0.37W 
1991 Nov 24    1434.29 35746 x 35756 x 12.4 GEO 73.5E+0.4W 
1998 Aug 2    1434.85 35742 x 35781 x 15.0 GEO 56.5W+0.31W 

Intelsat 303

  1969-011A


The Intelsat III F-3 satellite was launched in Feb 1969 and became the Pacific satellite. However only a few months later one of two tunnel diode amplifiers malfunctioned, and the satellite was replaced as Pacific primary by the newly launched Intelsat III F-4. It was then moved to become Intelsat's first Indian Ocean region satellite. It was to remain over the Indian Ocean for a decade until it was finally decommissioned in Dec 1979.


Intelsat III F-3 
 

DateTimeEventOrbit  

1969 Feb 6  0039:00 Launch by Delta M  CK LC17A 
  T+0:39 SRM 1-3 burnout 
  T+1:05 Castor sep 
 0042:38 T+3:38 MECO, 130 km 
 0042:38? St 1 sep 
 0042:45 T+3:45 SES 6:18 
 0043:00 T+4:00 Fairing 
 0049:03 T+10:03 SECO 
  Coast 9:52? 
  Stage 2 apogee 374 km  -484? x 374 x 32.7? 
   -504? x 375 x 32.5? 
 0058:40 T+19:40 St 2 sep 
 0058:54 T+19:54 Star 37D burn 41s at 278 km  
 0059:38 TECO  671.91 253 x 37813 x 29.8 
   638.0 265 x 36097 x 28.89  
 0101:20 T+22:20 Star 37D sep 
 0101:21  Yo weight sep 
 0630?  Apo 1 68E (short orbit) 
 0700? First apogee over 63E 
 1700?  Apo 2 90W (short orbit) 
 1800? Second apogee over 103W 
1969 Feb 7  0400?  Apo 3 107E (short orbit) 
1969 Feb 7  0500? Third apo over 88E 
 1400?  Apo 4 48W (short orbit) 
 1600? Apo 4 over 80W 
1969 Feb 8  0100? Apo 5 over 150E (short orbit) 
1969 Feb 8  0030? SVM-2 burn  
1969 Feb 8  0330? Apo 5 over 110E 
1969 Feb   POR satellite  GEO 174E 
1969 Feb 21   R/B orbit  236 x 36205 x 29.6  
1969 Mar 17    1436.46 35779 x 35808 x 1.3 GEO 174.39E+0.00 
1969 May?   Environmental control system issues 
1969 Jun 1  Replaced by III F4 in POR 
1969 Jun 2   At GEO 172.3E 
1969 Jun 3   Enter drift 5 deg/d to move to IOR 
1969 Jun 24?  IOR satellite  GEO 62.5E 
1969 Dec 1    1436.28 35777 x 35802 x 0.7 GEO 62.8E 
1971 May 25    1436.14 35783 x 35791 x 0.8 GEO 61.3E 
1975   IOR backup 
1975 Dec    GEO 56.5E (Morgan) 
1976 Sep   Replaced by IV F-1 
1977 Feb 24    1436.08 35777 x 35795 x 4.6 GEO 56.8E 
1977 May 20    GEO 56.0E+0.1E 
1977 Aug 4    GEO 54.8E 
1978 Sep   IOR contingency GEO 57.0E 
1979 Feb 1    GEO 60.0E 
1979 Feb 22   Drift east to 66E 
1979 Mar 28    GEO 66.0E 
1979 May 24    GEO 66.8E 
1979 Dec   GEO 66E 
1979 Dec 13  1400  Orbit raised  1674 
1979 Dec 14  0200  Decommissioned  
1980    1674.5 39735 x 40937 x 6.4 

May 13,2026

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