Thursday, April 19, 2001

Iridium MFS-1

 1997-048A


Two Iridium Mass and Frequency Simulators were launched on a CZ-2C from Taiyuan to demonstrate the capability of the CZ-2C launch vehicle and its new Smart Dispenser upper stage. The MFS were probably built by Motorola/Chandler, but are owned by China. The inert satellites, with a mass of around 650 kg, were designed to reproduce the mass distribution and oscillation frequency response of a real Iridium payload.

The apogee burn is about 125 m/s, while the reported capability of the SD is around 200 m/s with 125 kg propellant.


Iridium MFS 1 
 

DateTimeEventOrbit  

1997 Sep 1 1400:15  Launch  
 1402:17  T+2:02 Stage 1 cutoff 
 1402:17  T+2:02 Stage 2 burn 
 1402:17  T+2:02 Stage 1 sep 48 km  -6180 x 81? 
 1404:05  T+3:50 Fairing sep 117 km  -5560 x 120 ?  
 1405:17  T+5:02 Stage 2 MECO  -3000 x 150 ? 
 1410:25  T+10:11 Stage 2 VECO 
 1410:29  T+10:14 Stage 2 sep  177 x 615 x 86.3 
 1448:23  T+48:08 SD burn 
 1448:59  T+48:44 SD burnout 
 1450:18  T+50:03 SD sep 623 x 633 x 86.3  
 1454:09  T+53:54 SD deorbit  215 x 638 x 86.2  
1997 Sep 3    97.26 623 x 631 x 86.3 
1997 Sep 10    97.26 623 x 631 x 86.3 
1998 Mar 9    97.26 620 x 634 x 86.3 
2000 Jun 24    97.06 614 x 621 x 86.4 

Club Management: September-October 2000

 https://welib.org/md5/4c4ecd8eae44f647bb5811d1f0d1c0a0

The First Time

https://welib.org/md5/1d327af45bd699d0d43d7f72968af87d

Spaceflight: September 2000

 https://welib.org/md5/65e333357a448e74999addd7edb06424

Seventeen: October 2000

 https://welib.org/md5/0c91fdfa6e8904f0bde17d5e4982677e

Dawson’s Creek Omnibus

https://welib.org/md5/bced46e3deab7f895b311e18117cbe85

Wednesday, April 18, 2001

Westar 3

 1979-072A


Western Union's third domestic C-band satellite was launched in 1979. Westar III was stationed at 91 deg W. It was retired in 1990.


Westar 3 
 

DateTimeEventOrbit  

1979 Aug 10  0020  Launch by Delta 2914  CC LC17 
  T+3:48 MECO 
  T+3:56 St 1 sep 
  T+4:01 SES-1 4:54 
  Fairing 
 0028 T+8:55 SECO-1  88.18 130 x 239 x 31.47 
   88.18 130 x 239 x 28.5?  
 0042  T+22:37 St 2 sep 
 0043  T+23:20 Star 37E burn  
 0044  T+24:03 Star 37E burnout 231 x 36681 x 24.3  
 0045  T+25:15 Star 37E sep 
1979 Aug 11  1430  FW5 AKM burn 
1979 Aug 24    1443.79 35796 x 36077 x 0.16 GEO 81.3W+1.9W 
1979 Aug 31    1436.37 35774 x 35809 x 0.3 GEO 90.9W+0.08W 
1979 Sep 12    1436.03 35779 x 35790 x 0.2 GEO 90.7W 
1980 Jan 8    1436.15 35778 x 35796 x 0.0 GEO 91.1W 
1981 Jan 1    1436.11 35779 x 35793 x 0.0 GEO 90.9W 
1982 Jan 3    1436.12 35778 x 35795 x 0.0 GEO 91.0W 
1983 Jan 1    1436.14 35784 x 35790 x 0.0 GEO 91.0W 
1984 Jan 2    1436.15 35783 x 35791 x 0.0 GEO 91.1W 
1985 Jan 4    1436.10 35782 x 35790 x 0.0 GEO 91.0W 
1986 Jan 5    1436.11 35780 x 35793 x 0.0 GEO 91.0W 
1987 Jan 3    1436.12 35783 x 35791 x 0.0 GEO 90.9W 
1988 Jan 2    1436.08 35780 x 35792 x 0.0 GEO 90.9W 
1989 Jan 15    1436.12 35779 x 35794 x 1.0 GEO 91.1W 
1990 Jan 2    1436.09 35780 x 35793 x 1.9 GEO 90.9W 
1990 Jan 17    1436.12 35781 x 35792 x 2.0 GEO 90.9W 
1990 Jan 24   Orbit raise 1440.94 35878 x 35884 x 2.0  
1990 Mar 15  1440.79 35873 x 35880 x 2.9 

Landsat 1

  1972-058A


ERTS A was launched at 1806:06 on 1972 Jul 23 by a Delta from Vandenberg. The Delta solids separated at 1807:31 and the Thor stage at 1809:46. Delta 89 ignited at 1809:50 and cutoff at 1851:21, entering parking orbit. At 1903 the Delta restarted for an 11 second circularization burn and separated from ERTS A at 1916:41. At 1924 UT the Delta made a third burn, lowering its perigee to 635 x 910 km. ERTS 1 took its first pictures the following day. On 1973 Jan 14 the satellite was renamed Landsat 1, and it continued operating until 1978 Jan 26. Its images were used for crop forecasts, soil surveys, cartography, water supply studies, irrigation studies, geological prospecting, and monitoring of oil slick pollution.


ERTS 1 
 

DateTimeEventOrbit  

1972 Jul 23  1806:06  Launch by Delta  V SLC2W
  SRM 7-9 on at 6 km 
  SRM 1-6 burnout 
 1807:31  T+1:25 SRM 1-9 sep 
  T+3:38 MECO 
 1809:46  Thor sep 
 1809:50  Delta st 2 burn 5:31 
 1815:21  SECO-1  185 x 890 x 99 
 1903  SES-2 11s 
 1903  SECO-2 
 1916:41  St 2 sep  903 x 921 x 99.1 
 1924  SES-3 avoidance and restart test 
 1925?  SECO-3  635 x 910 x 98.5 (Delta) 
1972 Jul 24   First images 
1978 Jan 16   End of ops 

USA-108

 1995-003A


This was the first of the Block II UHF F/O series, with an EHF (Extremely High Frequency) package, requiring a switch to the more powerful Atlas II booster. The satellite had a mass of 3023 kg at orbit insertion, including 1673 kg of propellant.


UHF F/O F4 
 

DateTimeEventOrbit  

1995 Jan 29  0125  Launch from LC36A 
 0127:45  Booster sep 
  MECO at 160 km 
 0129  Centaur burn 1, 6:45 
 0135  Centaur MECO, 11 min drift  170 x 1598 km 
 0146  Centaur burn 2,  
 0148  Centaur MECO-2 
 0153  Centaur sep 
1995 Jan 29    479.42 301 x 27524 x 26.9 
1995 Jan 30  1745? LAM-1 at perigee 
1995 Jan 31    638.26 313 x 36042 x 26.7 
1995 Feb 1  0700?  LAM-2 apogee 
1995 Feb 1    781.74 7495 x 35698 x 14.7 
1995 Feb 2  0900?  LAM-3 
1995 Feb 2    1171.36 24473 x 36387 x 5.4 
1995 Feb 4  0100?  LAM-4 
1995 Feb 4    1400.47 34225 x 35947 x 5.2 
1995 Feb 4  2300?  LAM-5 
1995 Feb 7    1436.23 35645 x 35933 x 5.1 GEO 170.8W+0.04W 
1995 Feb 25    1436.02 35647 x 35923 x 5.1 GEO 170.1W 
1995 Mar 8   mv out 
1995 Mar 20    1436.77 35788 x 35810 x 5.1 GEO 176.6W+0.2W 
1995 Apr 21    1436.14 35776 x 35798 x 5.1 GEO 177.9W 
1995 Sep 9    1435.89 35768 x 35796 x 4.9 GEO 176.3W 
1995 Dec 20    1436.23 35772 x 35805 x 4.8 GEO 176.9W 
1997 Jun 17    1436.17 35775 x 35800 x 4.3 GEO 177.6W 
1999 Mar 23    1436.28 35772 x 35808 x 3.5 GEO 177.0W 

Monday, April 16, 2001

Kosmos 1178

 1980-036A



Kosmos-1178 
 

DateTimeEventOrbit  

1980 May 7  1300 Launch by Soyuz-U  Plesetsk 
 1308  Blok-I burn 
1980 May 7    90.36 195 x 389 x 72.9 
1980 May 8  0530? Orbit raise  92.26 356 x 414 x 72.9 
1980 May 21    92.26 357 x 412 x 72.9 
1980 May 22   
 0732?  Deorbit 
 0742? PO sep 
 0800?  Entry 
 0815? Landed 

Sakura 3B

 1988-086A


Sakura 3B (CS 3B) was launched in Sep 1988.


Sakura 3B 
 

DateTimeEventOrbit  

1988 Sep 16  0959:00 Launch by H-I  TNSC 
  T+0:39 SOB 1-6 out 
  T+0:40 SOB 7-9 on 
  T+1:19 SOB 7-9 out 
  T+1:25 SOB 1-9 sep 
  T+4:26 MECO 
  T+4:32 VECO 
  T+4:34 St 1 sep 
 1003 T+4:39 SES 
 1004 T+5:04 Fairing 
 1009 T+10:37 SECO 
 1023 T+24:00 Spinup 
 1023 T+24:05 Stage 2 sep  89.85 198 x 336 x 30.72 
 1023 T+24:28 Stage 3 burn 
 1024 T+25:30 TECO 
 1025 T+26:30 Stage 3 sep  662.7 199 x 37405 x 28.3 (NASDA) 
 1025 T+26:32 Stage 3 tumble 
 1600? Apo 1 
 2130? Peri 1 
1988 Sep 17  0330? Apo 2 
 0830? Peri 2 
 1400? Apo 3 
 1930? Peri 3 
1988 Sep 18  0100? Apo 4 over 175E 
1988 Sep 18  0054:17 Star 30B burn 
  over 167E? 
1988 Sep 18    1465.88 35519 x 37217 x 0.31 
1988 Sep 20    1451.0 35559 x 37159 x 0.21 (NASDA) 
1988 Sep 20    1452.04 35613 x 36583 x 0.23 
1988 Sep 21    1439.61 35646 x 36064 x 0.23 
1988 Sep 23    1433.69 35614 x 35864 x 0.20 GEO 145E+0.5/d 
1988 Sep 28    1432.27 35596 x 35827 x 0.16 GEO 148E+1/d 
1988 Oct 2    1435.98 35762 x 35805 x 0.2 GEO 149.2E 
1988 Oct 8   On sta for tests 1436.06 35784 x 35788 x 0.16 GEO 149.0E 
1988 Nov 9    1436.14 35785 x 35789 x 0.1 GEO 148.9E 
1988 Nov   Move to 136E 
1988 Nov 28    1436.15 35783 x 35791 x 0.1 GEO 135.9E 
1989 Jul 31    1436.16 35777 x 35798 x 0.1 GEO 136.1E 
1990 Oct 4    1436.13 35785 x 35789 x 0.0 GEO 136.0E 
1992 Jan 12    1436.17 35785 x 35790 x 0.0 GEO 135.9E 
1993 Jun 4    1436.11 35786 x 35787 x 0.0 GEO 136.0E 
1996 Jan 4    1436.13 35779 x 35794 x 0.0 GEO 136.0E 
1997 Feb 8    1436.15 35777 x 37597 x 0.0 GEO 135.9E 

STS-38 (Atlantis)

 1990-097A


The STS-38 mission was a classified military satellite deployment mission. Of all the STS military flights, this one is possibly the most mysterious.

The OMS-1 burn occurred at an altitude of around 120 km. It probably had a magnitude of 30-35 m/s based on the duration. The angle is unknown, but plausible solutions are to keep the angle or the perigee constant. If the angle is constant (dVx = 30-35, dVz = 0) the orbit is 16-27 x 164-169 km. If the perigee is constant (dVx=17-20, dVx=25-29) the orbit is 73 x 162-170 km. If the apogee is constant the perigee is implausibly high. The ET reentered in the Indian Ocean at 28.5S 84.9E, similar to other non-direct-ascent flights, and most likely the perigee was on the low side: I adopt 20 x 165 km as a plausible post-MECO orbit.

The Shuttle made an RCS and an OMS burn to raise the orbit to 263 x 272 km, and presumably this was the orbit from which payload deployment occurred (unless the OMS was a post-deploy separation burn, but it seems a bit large for this).

The AFP-658 payload was deployed on Nov 16. On Nov 17, the perigee was lowered to 222 km, either for Earth observations or to optimize landing opportunities. Landing was on Nov 20.


STS-38 
 

DateTimeEventOrbit  

1990 Jun 8   Tow to VAB 
1990 Jun 9   ET mate  VAB 
1990 Jun 18   Rollout  LC39A 
1990 Aug 8   Rollback to outside VAB 
1990 Aug 9   Rollback to VAB  VAB/3 
1990 Aug 15  Demate  VAB/3 
1990 Aug 16   Tow to OPF  OPF/2 
1990 Oct 2   Tow to VAB  VAB/3 
1990 Oct 4   ET mate  VAB/3 
1990 Oct 12   Rollout  LC39A 
1990 Nov 15  2348:15  Launch from LC39A 
 2350:18  SRB sep 
 2356:44  MECO 
 2357:02  ET sep  86.29 20 x 165 x 28.45 
 2358:45  OMS-1 (75s) 30-35m/s??  
1990 Nov 16  0000:07  OMS-1 CO  87.44 73 x 221 x 28.45  
1990 Nov 16  0025:48  OMS-2 (103s) 40m/s?  
 0027:21  OMS-2 CO 
 0122:23  PLBD open 
 0041   88.89 215 x 223 x 28.47 
 0100   88.87 214 x 223 x 28.47 
 0335  At perigee 28S 47E 
 0425At apogee 26N 125W 
 0430?  RCS burn 
 0500 89.36 217 x 267 x 28.47 
 0528:23  OMS-3 30s burn 
 0528:53  OMS-3 CO 
 0656?  AFP-658 deployed 
 0716  RCS sep? 
 0948   89.87 263 x 272 x 28.46 
 2322   89.88 264 x 272 x 28.46 
1990 Nov 17  0437?  PROWLER deploy 
 0456?  RCS sep? 
 1249   89.80 260 x 269 x 28.47 
 2119:45  OMS-4 20s
 2120:05  OMS-4 CO 
 2120   89.39 222 x 266 x 28.47 
1998 Nov 18  0718   89.38 221 x 265 x 28.47 
 2134   89.35 220 x 264 x 28.47 
1990 Nov 19  1448   89.34 220 x 263 x 28.48 
1990 Nov 19  2035Landing waved off
1990 Nov 20  0147   89.32 219 x 262 x 28.48 
1990 Nov 20  1811   89.31 219 x 261 x 28.47 
 1916:46  PLBD closed 
 2046:15  OMS DO 1:55 70m/s 
 2048:09  OMS DO CO 
 2111:52  Entry 
 2142:42  Landed KSC RW33 
 2142:52  NGTD 
 2143:41  Wheels stop 
1990 Nov 21 0130Tow to OPF/2 

Sunday, April 15, 2001

Kupon

 1997-070A


The Kupon K95K satellite was owned by Global Information Systems of Moscow, a subsidiary of the Russian Federal Central Bank. It was based on Lavochkin's Geizer system and was stationed at 55E. It provided financial data relay for the Bankir network, relaying info from HQ to a network of VSAT dishes. The phased array antenna allows coverage of different areas. Kupon's attitude control system failed unexpectedly in Mar 1998. The TsBank then transferred traffic to Intelsat 704 and two Russian comsats.


Kupon (K95K) 
 

DateTimeEventOrbit  

1997 Nov 12 1700 Launch by Proton/DM-2M 
 1709 Stage 3 sep 
 1709  Adapter sep  184 x 190 x 51.6 
 1817? DM burn 1 
  DM MECO-1  200? x 36000? x 48.0 
 2331? DM burn 2 
 2340? DM sep 
1997 Nov 12    1450.22 36032 x 36093 x 0.0 GEO 91.4E+3.5W 
1997 Nov 20    1446.84 35672 x 36320 x 0.0 GEO 64.0E+2.7W 
1997 Dec 14    1436.10 35775 x 35798 x 0.0 GEO 54.9E 
1998 Mar   end of ops
1998 Apr 4    1435.98 35772 x 35796 x 0.0 GEO 55.3E 
1998 Jun 15    1435.66 35766 x 35789 x 0.2 GEO 60.2E+0.1E 
1999 Oct 16    1436.75 35795 x 35803 x 1.2 GEO 73.7E+0.2W

May 13,2026

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