Monday, May 2, 2016

Echostar 4

 1998-028A


Echostar 4, an A2100AX, used an ILS Proton launch. DM3 stage No. 7L placed the satellite in GTO. Mass was 3470 kg full, 1580 kg dry. Bus is 1.8 x 1.8 x 4.5m with 21m span.

Echostar 4 was intended to replace Echostar 1 at 119W (Echostar 1 would go to 148W). It was to become the primary DISH network provider to the US together with Echostar 2, with Echostar 1 and 3 providing local, educational, business and data transmission services for Echostar Satellite Services. However, two of five solar panels on one array did not unfold, limiting power; Echostar claimed a loss on the insurance. An insulation material melted during transfer orbit coast and glued the arrays in their folded position. Echostar was placed at 148W for local and educational broadcasting. In 1999 Echostar 4 was moved to 110W, starting off a new Dish Network service pending the launch of Echostar 5. Then, on 2004 Sep 4 the stuck solar array panels unexpectedly popped open, restoring full power.

In 2005, E4 was moved to 77E to provide service for Mexican company QuetzSat, partly owned by Echostar. It was replaced there by Echostar 1 and 8.


Echostar 4 
 

DateTimeEventOrbit  

1998 May 7  2345:00  Launch by Proton 393-02 KB 
  T+02:02 Stage 2 burn 
  T+02:06 Stage 1 sep 
  T+05:35 Stage 2 MECO, Stage 2 sep 
  T+05:40 Stage 3 burn 
  T+05:44 Fairing sep 
 2354:38 T+09:38 Stage 3 MECO 
  T+09:49 Stage 3 vernier cutoff 
 2354:49 T+09:49 Stage 3 sep 
 2355:44 T+10:44 Adapter sep 
1998 May 8  0059:19 T+1:14:19 DM burn 1 
 0105:52 T+1:20:52 DM MECO  629.71 213 x 35702 x 48.5 
 0603:55 T+6:18:55 DM burn 2  
 0605:45 T+6:20:45 DM MECO  8318 x 35750 x 15.3 (ILS)  
 0625:32 T+6:40:32 DM sep 
1998 May 8    794.47 8346 x 35727 x 15.4 
1998 May 9  2130?  LAM-1 
1998 May 11    878.46 12263 x 35747 x 10.6 
1998 May 13  1430? LAM-2 
1998 May 14    1079.10 21204 x 35739 x 4.7 
1998 May   Solar panel deploy problem 
1998 May 15?  LAM burn 
1998 May 18?   LAM burn  
1998 Jun 2    1436.10 35778 x 35795 x 0.0 GEO 127.0W 
1998 Jul 14    1436.12 35782 x 35792 x 0.0 GEO 127.0W 
1998 Jul 16   mv out 1440.86 35813 x 35946 x 0.0 GEO 128.0W+2.0W 
1998 Jul 29   mv in  
1998 Aug 15    1436.10 35782 x 35791 x 0.0 GEO 148.0W 
1999 Jun 10    1436.04 35775 x 35795 x 0.1 GEO 147.8W 
1999 Jun   Relocate to 110W  
1999 Jul 29    1436.09 35780 x 35792 x 0.1 GEO 110.1W 
1999 Oct 16    1436.06 35778 x 35793 x 0.1 GEO 110.1W 
1999 Dec 22    GEO 110.5W 
2000 Jan 20   Mv in  GEO 119.5W 
2000 Jun 13    1436.13 35775 x 35798 x 0.0 GEO 119.5W 
2003 May 16   mv out  GEO 119W 
2003 Jul 20   mv in  GEO 157W 
2004 Sep 4   Solar panels pop open 
2005 May 27    1436.13 35773 x 35800 x 0.8 GEO 157.0W 
2005 Jun 18   mv out  1436.06 35776 x 35794 x 0.8 GEO 157.0W 
2005 Jul 6   mv in at 77W (Quetzsat) 
2005 Jul 16    1436.20 35779 x 35797 x 0.9 GEO 76.8W 
2006 Aug 4    1436.11 35771 x 35802 x 0.6 GEO 77.0W 
2011 Jul 11    1436.11 35768 x 35804 x 2.8 GEO 76.7W 

Zhongwei 1

 1998-033A


The China Orient Telecommunications Satellite Co. of Beijing (part of the Ministry of Posts and Telecommunications) contracted Lockheed Martin Astro Space to build the A2100 class Zhongwei I (Chinastar 1). The satellite was launched in the spring of 1998 by CZ-3B and has a mass of 2984 kg (1418 kg BOL). It will serve China, southeast Asia, India and Korea. It entered a supersynchronous orbit, later lowered to geostationary. However, the orbit remained eccentric.

China Orient was later merged into China Satcom and Zhongwei 1 was renamed Zhongxing 5A. China DBSAT was founded Dec 2007 and merged into China Satcom in Apr 2009.


Zhongwei 1 
 

DateTimeEventOrbit  

1998 May 30  1000  Launch by CZ-3B 
  T+2:07 Booster sep 
  T+2:27 St 1 sep 
  T+3:52 Fairing 
  T+5:32 St 2 sep 
  T+5:32 St 3 MES-1 
 1010 T+10:31 MECO-1  160? x 450? x 28.5? 
 1021 T+21:21 MES-2 
 1024 T+24:20 MECO-2 
 1026? T+26:00 Stage 3 sep  216 x 85035 x 24.4 
1998 May 31    1799.28 216 x 85033 x 24.4 
1998 May 31  0120 First apogee at 127E 
1998 Jun 1  0720  Second apogee at 36E 
1998 Jun 2  1320  Third apogee at 54W, LAM-1 
1998 Jun 3    2337.39 14468 x 89459 x 7.0 
1998 Jun 4  0300  Fourth apogee at 97E 
1998 Jun 5  1753  Apogee 5 at 128W 
1998 Jun 6?   LAM burn 
1998 Jun 6    2860.72 35759 x 84992 x 1.3 
1998 Jun 8  1340  LAM at perigee 
1998 Jun 8    2203.06 35731 x 63682 x 1.0 
1998 Jun 11  1500? LAM at perigee 
1998 Jun 13    1435.00 35678 x 35851 x 0.1 GEO 86.9E+0.3E 
1998 Jun 15    1435.60 35742 x 35811 x 0.1 GEO 87.5E+0.1E 
1998 Jun 30    1436.16 33915 x 37661 x 0.09 
1998 Jul 20    1436.14 35779 x 35795 x 0.0 GEO 87.5E 
1999 Oct 18    1436.07 35776 x 35795 x 0.0 GEO 87.6E 
2006 Aug 3    1436.11 35774 x 35799 x 0.1 GEO 87.6E 
2013 Aug 10    1436.06 35768 x 35803 x 0.0 GEO 87.6E 

May 13,2026

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