Saturday, December 22, 2007

Intelsat 804

 1997-083A


Intelsat 804 was launched to the IOR position, covering Asia, Europe and Africa. Mass is 3455 kg launch, 2079 kg BOL, 1601 kg dry. The bus is 2.5 x 2.2 x 5.2 m with 10.8m solar panel span. Location was be 64 E (IOR); it was moved to the Pacific 176E location in 2002 and then to the 174E location (replacing I-802) in 2004. 


Intelsat 804 
 

DateTimeEventOrbit  

1997 Dec 22  0017  Launch by Ariane 42L (V104) 
 0019  T+02:36 PAL sep 
 0020  T+03:23 St 1 sep 
 0021  T+04:13 Fairing sep 
 0022  T+05:41 St 2 sep 
 0022  T+05:50 St 3 burn 
 0035  T+18:51 St 3 cutoff 
 0037  T+20:46 St 3 sep
 0040  T+23:41 St 3 depletion
1997 Dec 22    631.81 363 x 35760 x 7.0 
1997 Dec 23??  LAM-1  
1997 Dec 25??  LAM-2
1997 Dec 29    1436.11 35767 x 35805 x 0.1 GEO 47.0E 
1998 Jan 21    1435.93 35776 x 35789 x 0.1 GEO 47.0E 
1998 Jan 25   mv out 
1998 Feb 3   mv in  1436.11 35774 x 35798 x 0.1 GEO 64.1E 
1999 Oct 17    1436.07 35767 x 35804 x 0.0 GEO 64.1E 
2002 Oct 19    1436.07 35771 x 35800 x 0.0 GEO 64.1E 
2002 Oct   Move to Pacific  
2002 Dec 4    1436.08 35772 x 35799 x 0.1 GEO 176.0E 
2004 Aug 3   mv out 1436.10 35768 x 35804 x 0.1 GEO 176.0E 
2004 Aug 27    1436.09 35771 x 35801 x 0.0 GEO 174.0E

Thursday, December 20, 2007

USA-114

 1995-057A


UHF F6, the third UHF F/O Block II satellite, was launched by Atlas II from Cape Canaveral on 1995 Oct 22. It had a launch mass of 3017 kg and was stationed at 100W, replacing Leasat 3.


UHF F/O F6 
 

DateTimeEventOrbit  

1995 Oct 22  0800:02  Launch by Atlas II (AC-119) 
 0802  BECO 
 0802  Booster sep 
 0803  Fairing sep 
 0804  SECO 
 0804  Atlas sep 
 0805  Centaur AC-119 MES1 
 0811 Centaur AC-119 MECO1 
 0822?  Centaur AC-119 MES2 
 0824? Centaur AC-119 MECO2 
 0827? Centaur AC-119 sep  551.9 320 x 31500 x 27.0 
 0845?Centaur AC-119 depletion  478.1 267 x 27483 x 27.0 (AC-119) 
1995 Oct 22    482.12 276 x 27701 x 27.0 
1995 Oct 23  1630?  LAM-1 perigee 
1995 Oct 23    551.94 320 x 31500 x 27.0 
1995 Oct 25  0100?  LAM-2 apogee 
1995 Oct 25    798.58 7657 x 36612 x 14.6 
1995 Oct 26  1630? LAM-3  
1995 Oct 27    1151.13 23391 x 36620 x 7.3 
1995 Oct 28  0630?  LAM-4 
1995 Oct 28    1411.73 34033 x 36583 x 5.3 
1995 Oct 29  0800?  LAM-5 
1995 Oct 29    1430.25 34761 x 36583 x 5.3 GEO 170.4W+1.4E 
1995 Nov 6    1436.02 34984 x 36585 x 5.1 GEO 171.4W 
1995 Nov 22    1435.98 34979 x 36589 x 5.1 GEO 172.1W 
1995 Nov 27   mv out 
1995 Dec 18    1436.05 35773 x 35798 x 5.0 GEO 105.3W 
1996 Apr 14    1436.09 35773 x 35799 x 4.9 GEO 105.4W 
1998 Jan 29    1436.12 35776 x 35797 x 4.2 GEO 104.7W 
1999 Jul 29    1436.09 35774 x 35798 x 3.5 GEO 105.9W 
2005 May 12    1436.12 35771 x 35802 x 9.0 GEO 104.5W 

Wednesday, December 19, 2007

Progress M-59

 2007-002A


PM-59 11A615A55 No 359 Soyuz U, flight 24P. Mass 7274 kg. Cargo 2561 kg, 1390 in GO.


PM59 
 

DateTimeEventOrbit  

2007 Jan 18  0212:15  Launch by Soyuz-U No. Ts15000-107 
 0220:58  T+8:45 Blok-I MECO 
 0221:04  T+8:49 Blok-I Sep 
 0610:18  DV1 11.8m/s 
 0640:27  DV2 13m/s 
2007 Jan 19  0257:08  DV3 1.0m/s 
2007 Jan 20  0102:06  DV4 22m/s 
 0125:21  DV 0.8m/s 
 0146:16  DV 17.6m/s 
 0227:43  DV 7.1m/s 
 0232:41  DV 5.0m/s 2.6km range 
 0235:11  DV 2.2m/s 1.0km range 
 0236  Begin flyaround  
 0244  Complete flyaround at 170m 
 0250  Approach  
 0258:53  Docked with Pirs 
2007 Aug 11407:05  Undocked from Pirs 
 1842  Deorbit burn 
 1927  Impact in Pacific 

May 13,2026

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