Thursday, November 18, 1993

Molniya 166

 1985-103A


Molniya-1 (F72, N66) was launched on 1985 Oct 27 from Plesetsk, within a few days of the previous Molniya-1 launch from Baikonur. 


Molniya-1 F72 
 

DateTimeEventOrbit  

1985 Oct 28  1724:58  Launch by 8K78M  PL 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 1733  T+8:50 Blok-I sep 
  T+53:16 BOZ burn 
 1819?  T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 1822?  T+56:54 ML sep   
1985 Oct 28    460 x 39132 x 62.8 

Molniya 131

 1975-079A


Molniya-1 (F36, N31) was launched on 1975 Sep 2 into the C plane. It replaced F33.


Molniya-1 F36 
 

DateTimeEventOrbit  

1975 Sep 2  1309 Launch by 8K78M  PL 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 1317  T+8:50 Blok-I sep 
  T+53:16 BOZ burn 
 1402?  T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 1405?  T+56:54 ML sep   
1975 Sep    736.7 623 x 40667 x 62.9 
1975 Sep    717.8 606 x 39749 x 62.9 
1986 Nov 19   Reentered 

Intelsat 402

  1971-006A


The first Intelsat IV, F-1, was kept in storage until 1975. F-2 was the first to be launched, and was primary Atlantic satellite from 1971 to Sep 1973 when it was replaced by F7. It remained over the Atlantic in a backup role until it was switched off in 1983.


Intelsat IV F-2 
 

DateTimeEventOrbit  

1971 Jan 26  0036:03 Launch by Atlas Centaur  CC LC36 
  T+2:32 BECO 
  T+2:35 Booster sep 
  T+3:17 Insulation panels 
  T+3:58 SECO, VECO  
 0040 T+4:01 Atlas sep 
  T+4:12 Centaur MES-1 
  T+4:24 Fairing 
 0046 T+10:18 Centaur MECO-1  109.83 185 x 2252 x 29.4 
 0100? T+24? Centaur MES-2 
 0101? T+25? Centaur MECO-2 
 0104 T+28:47 Centaur sep 640.52 547 x 35924 x 28.2 
 0700?  Apo 1 
 1800?  Apo 2 
1971 Jan 27  0330? Apo 3 over 125E 
1971 Jan 27  0344  AKM 3.6W/d 
1971 Mar 26   Operational, AOR Primary with III F7  GEO 24.5W 
1971 Apr 22    1436.34 35785 x 35797 x 0.5 GEO 34.3W+0.07E 
1971 Oct 25    1436.04 35775 x 35796 x 0.1 GEO 23.4W 
1972   AOR Primary 
1973 Sep   Replaced by IV F7 
1975 Dec    GEO 19W (Morgan) 
1976 Feb   AOR Backup  GEO 1W 
1977 Feb 26    1435.98 35770 x 35798 x 0.02 GEO 5.1W 
1977 Dec    GEO 4W (Morgan) 
1978 Mar 27    1436.13 35781 x 35793 x 0.82 GEO 4.8W 
1978 Sep   AOR Backup  GEO 4W 
1979 Apr   Available as backup GEO 6W 
1979 Oct   mv in  GEO 4W 
1979 Oct 12    1435.93 35777 x 35789 x 1.9 GEO 3.6W 
1980 Mar 3    1436.02 35779 x 35790 x 2.2 GEO 3.7W 
1980 May   mv out  GEO 4W 
1980 May   mv in  GEO 1W 
1980 May 30    1436.02 35773 x 35796 x 2.3 GEO 0.4W 
1982 Aug 9   mv out  GEO 1W 
1982 Aug 27    1435.97 35776 x 35792 x 4.0 GEO 0.5E 
1982 Oct   Engineering tests  GEO 3E 
1982 Dec 19    1436.27 35766 x 35813 x 4.3 GEO 3.83E 
1983 May 10    1435.89 35752 x 35812 x 4.6 GEO 4.6E 
1983 May 11   Orbit raise 300 km  35969 x 36009 
1983 May 11   Decommissioned 
1983 May 12    1446.26 35965 x 36005 x 4.6 
1985 Nov 16    1456.88 36121 x 36261 x 6.7 
1986 Dec 3    1456.90 36125 x 36259 x 7.6 
1998 Aug 5    1456.96 36115 x 36272 x 15.1 

Monday, November 15, 1993

Nova 3

 1984-110A


Nova 3 (NNS 30500) was launched in Oct 1984. Its mass was 120 kg (or 166 kg).

Mass 173 kg (MOR). Mass at St 4 burnout 210 kg; St 4 ignition 486 kg. Conclude St 4 is mass 313 full 37 empty.

1.1m high 0.52m dia cyl bus with 4 panels and 79.2m gravity boom. Despin via magnets?


Nova 3 
 

DateTimeEventOrbit  

1984 Oct 12  0143:34 Launch by Scout  V SLC5 
  T+1:23 St 1 burnout 
 0145:02 T+1:28 St 1 sep 
 0145:09 T+1:35 St 2 burn  -6302 x 63 x 76.9 
 0145:40 T+2:06 St 2 burnout 
 0146:10 T+2:36 St 2 sep  -5831 x 166 x 86.3 
 0146:14 T+2:40 Fairing sep-5831 x 166 x 86.3 
 0146:16 T+2:42 St 3 burn 
 0147:04 T+3:30 St 3 burnout  -4040 x 339 x 89.1 
  T+7:30 St 1 impact 
 0151:35 T+8:01 St 3 sep 
 0151:40  T+8:06 St 4 burn, 33s  -4040 x 335 x 89.1 (MOR) 
 0152:13 T+8:39 St 4 burnout  334 x 1007 x 90.0 (MOR) 
 0155? St 4 sep 
  T+11:16 St 2 impact 121.3W 24.2N 
  T+19:02 St 3 impact at 123.0W 1.63S 
1984 Oct 13   Activate DISCOS  323 x 1053  
  Orbit raise  357 x 1064 
1984 Oct 15    102.21 648 x 1076 x 89.8  
1984 Oct 16    104.32 818 x 1104 x 89.8 
1984 Oct 17    1023 x 1157 x 89.9 
1984 Oct 19    1160 x 1200 x 90.0 
1984 Nov 10  0400  Op frequency on 
1993 Nov 8  0237  Retired from service 

Sunday, November 14, 1993

Kosmos 453

 1971-090A


 Kosmos-453 was a subgroup 1 DS-P1-Yu mission launched in Oct 1971 by 11K63 from Plesetsk.


Kosmos-453 
 

DateTimeEventOrbit  

1971 Oct 19  1240  Launch by 11K63  PL 
 1242 Stage 2 burn  
 1247? Stage 2 sep  
1971 Oct 26  0500   92.19 271 x 493 x 71.0 (RAE) 
1972 Jan 1  0000   91.47 259 x 434 x 71.0 (RAE) 
1972 Mar 3  End of operations 
1972 Mar 19  0155? Reentered 

Interkosmos 18

 1978-099A


The Magnetospheric Interkosmos (Mag-IK) satellite was launched on 1978 Oct 24 by Kosmos-3M from Plesetsk. The satellite was named Interkosmos-18 once in orbit. The lead science institute for the Interkosmos-18 project was IZMIRAN, the Institute of Terrestrial Magnetism and Aeronomy of the Academcy of Sciences. Interkosmos-18 carried a set of particles and fields instruments to study the magnetosphere in the 400 to 800 km altitude range. It also ejected the Czechoslovak satellite Magion to provide comparative data. Mag-IK operated until reentry in Mar 1981.

Mass was 990 kg.


Interkosmos-18 
 

DateTimeEventOrbit  

1978 Oct 24  1900  Launch by 11K65M Kosmos-3M  NIIP-53 
 1902  Stage 1 sep 
  Stage 2 burn 
 1908? Stage 2 MECO 
 1930? Stage 2 MECO-2 
   96.4 406 x 764 x 83.0 
1981 Mar 15 End of transmissions 
1981 Mar 17   Reentered 

Payload:

  • SG-R1 magnetometer

  • Low energy particle flux

  • Particle angular distances

  • Electric and magnetic fields

  • Double probe investigation of electrostatic fields

  • Electron and ion densities and temperatures

May 13,2026

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