Saturday, January 24, 1998

STS-47 (Endeavour)

 1992-061A


Endeavour's second flight was the Spacelab-J mission. This mission was funded by NASDA, the Japanese National Space Development Agency. The 8-day flight was devoted to scientific experiments in the Spacelab module (see Spacelab-J entry for details of the experiments). A truss carrying a set of Getaway Special canister experiments was also carried. The mission was notable as having the first crew to include a black woman, Dr. Mae Jemison. Dr. Jemison, after leaving NASA, also had a brief cameo on an episode of Star Trek - The Next Generation, becoming the first Trek extra to have actual spaceflight time on their resume.


STS-47 
 

DateTimeEventOrbit  

1992 Aug 17   Tow to VAB  
1992 Aug 21   ET mate  VAB/3 
1992 Aug 25   Rollout  LC39B 
1992 Sep 12  1423:00  Launch from LC39B 
 1425:04  SRB sep 
 1431:33  MECO  87.87 30 x 307 x 57.0 (OMS dV) 
 1431:52  ET sep 
 1433  RCS sep 
 1459:12  OMS-2 2:39 80m/s 90.61 298 x 310 x 57.0 
 1501:51  OMS-2 CO 
 1558  PLBD open 
 1634  Activate SL 
1992 Sep 13  0600   90.61 298 x 310 x 57.0 
1992 Sep 15    90.60 297 x 309 x 57.0 
1992 Sep 20  0143  Deactivate SL 

0915PBD closed  90.56 296 x 308 x 57.0 
 1152:20  OMS deorbit 2:33 80m/s 
 1154:53  OMS DO CO 
 1221:43  Entry interface 
 1253:22  Landing KSC RW33 
 1253:41  NGTD 
 1254:11  Wheels stop 
 1630Tow to OPF/1 


    STS-47 Crew

  • Commander Capt. Robert L. Gibson, USN

  • Pilot Maj Curtis L Brown, Jr, USAF

  • Payload Commander/MS1 Lt Col Mark C. Lee, USAF

  • Mission Specialist 2 Dr. Jay Apt, PhD, NASA

  • Mission Specialist 3 Dr. N. Jan Davis, PhD, NASA

  • Mission Specialist 4 Dr. Mae C. Jemison, MD, NASA

  • Payload Specialist 1 Dr. Mamoru Mohri, PhD, NASDA

ECS-2

 1984-080A


The NEC/Hughes GMS-3A satellite was launched in Aug 1984 and became Himawari 3.


Himawari 3 
 

DateTimeEventOrbit  

1984 Aug 2  2030 Launch by N-2  TNSC 
  T+0:38 SRM 7-9 on 
  T+1:15 SRM 1-9 sep 
  T+4:32 MECO  
  T+4:40 St 1 sep 
 2034  T+4:46 Stage 2 burn 
  T+5:00 Fairing 
 2041  T+11:07 SECO 
 2053 T+23:07 SES-2 7s 
 2053 T+23:14 SECO-2 
 2054  T+24:14 Spinup 
 2054 T+24:22 Stage 2 sep 
 2054  T+24:54 Stage 3 burn 37s? 
 2055 T+25:38 Stage 3 burnout after 44s 
 2056  T+26:54 Stage 3 sep 
1984 Aug 3  0300? Apo 1 
 0800? Peri 1 
 1300? Apo 2 
 1830? Peri 2 
1984 Aug 4  0000? Apo 3  
 0530? Peri 3 
 1100? Apo 4 at 178E 
1984 Aug 4  1100? Star 27 AKM at 4th apo 
1984 Aug 4  1105? Star 27 ejected 
1984 Aug 4    1451.05 35730 x 36427 x 1.9 GEO 178.9W+3.7W 
1984 Aug 13    1450.24 35784 x 36341 x 1.9 GEO 147.0E+3.5W 
1984 Aug 15?  Radiometer cover jettison 
1984 Aug 15?  mv in 
1984 Sep 7    1436.17 35782 x 35793 x 1.8 GEO 140.3E 
1984 Sep 27   Begin operational data 
1985 Jan 26    1436.12 35784 x 35789 x 1.4 GEO 140.3E 
1986 Jan 25    1436.20 35785 x 35792 x 0.5 GEO 139.8E 
1987 Jan 5    1436.02 35784 x 35786 x 0.4 GEO 140.0E 
1988 Feb 11    1436.04 35782 x 35788 x 0.7 GEO 140.1E 
1989 Feb 11    1436.26 35786 x 37593 x 0.8 GEO 139.7E 
1989 Dec 8    1436.34 35787 x 35795 x 1.4 GEO 139.0E+0.07W 
1989 Dec?   Move to 120E 
1990 Feb 14    1436.15 35786 x 35789 x 1.6 GEO 120.0E 
1991 Jan 1    1436.09 35784 x 35788 x 2.4 GEO 120.2E 
1993 Feb 22    1436.15 35782 x 35792 x 4.2 GEO 120.1E 

Seventeen: August 1997

 https://welib.org/md5/91bfebc59ece7030e906faa36d514770

Thursday, January 22, 1998

The Internet Directory

https://welib.org/md5/7e928f8bbce65202a098dbc4c7513954

Kosmos 1700

 1985-102A


The first Luch satellite was launched in Oct 1985 and operated over 95E.


Kosmos-1700 
 

DateTimeEventOrbit  

1985 Oct 25  1545  Launch by Proton  KB 
 1554  Stage 3 sep  192 x 218 x 51.6  
 1702?  DM burn 1  326 x 35761 x 47.5 
 2220?  DM burn 2 
 2224?  DM sep 
   1434.25 35671 x 35829 x 1.5 GEO 90.7E+0.5E 
1985 Nov 3   mv in  1435.98 35754 x 35813 x 1.4 GEO 94.7E+0.02E 
1985 Nov 13    1435.97 35758 x 35809 x 1.4 GEO 95.0E 
1986 Mar 4    1435.95 35779 x 35788 x 1.1 GEO 94.8E 
1986 Jul 20    1436.13 35777 x 35797 x 0.9 GEO 95.3E+0.02W 
1986 Aug 29   last mv 1436.18 35766 x 35809 x 0.7 GEO 94.2E+0.03W 
1986 Oct 18    GEO 91.5E+0.1/d 
1987 Feb 22    1436.75 35772 x 35826 x 0.2 GEO 74.3E+0.2W 
1989 Apr 1    1436.74 35776 x 35722 x 1.8 GEO 73.5E+0.2W 
1991 Mar 17    1436.70 35766 x 35829 x 3.6 GEO 81.7E+0.2W 
1995 Nov 6    1436.45 35775 x 35811 x 7.2 GEO 58.8E+0.1W

Nimbus 5

  1972-097A


Nimbus E was the first Nimbus satellite to be launched on a Delta. The Delta model 0900 launch vehicle ignited at 0756 on 1972 Dec 11; 35 seconds later the solid motors separated. Stage 1 separation occurred at T+3 min 48 sec, followed by a 3 min 52 sec Delta stage burn into transfer orbit, achieved at 0805 UT. At 0853 the Delta stage re-ignited to circularize the orbit, and separated from the payload at 0857. Nimbus E was now Nimbus 5, in a 1089 x 1102 km x 100.0 deg orbit. The Delta stage made two test burns and ended up in a more eccentric 1105 x 1528 km orbit. Nimbus 5 carried on sending back data until 1983 Apr 1.


Nimbus 5 
 

DateTimeEventOrbit  

1972 Dec 11  0756:00  Launch by Delta 0900  
  SRM sep 
  T+3:53 MECO 
  T+3:48? St 1 sep 
  T+4m? SES-1 5:12 
 0805? SECO-1  180? x 1100? x 99 
 0853  T+57:05 SES-2 12s 
 0853  SECO-2 
 0857  St 2 sep 106.87 1062 x 1101 x 99.9  
 0912? SES-3 experimental 
 0912? SECO-3 
 0927? SES-4 experimental 
 0927? SECO-4  1102 x 1519 x 99.8 (Delta) 
1972 Dec 11    106.87 1062 x 1101 x 99.9  
1983 Apr 1   End of ops 

Kosmos 379

  1970-099A


T2K No. 1 was launched in Nov 1970 as Kosmos-379. The modified 11A511L Soyuz-L launch vehicle placed the spacecraft in a typical Soyuz-type parking orbit. The T2K consisted of the cabin, including the Blok E propulsion system, and a lower section containing the landing gear.


 Kosmos 379
 

DateTimeEventOrbit  

1970 Nov 24  0515:01  Launch by 11A511L  KB  
 0520?  Blok-I burn  
 0524?  Blok-I sep  
 0700   88.61 189 x 222 x 51.67 (TLE)  
 0930   88.78 191 x 237 x 51.61 (TLE)  
 2130   88.67 192 x 232 x 51.62 (RAE)  
1970 Nov 25  1430?  LK Blok-E burn  98.79 196 x 1206 x 51.65  
  Simulated lunar descent and hover 
1970 Nov 26   Ion flux meter turned on 
1970 Nov 27  0805?  Landing gear jettison 98.63 188 x 1198 x 51.59 
1970 Nov 28  0515?  Blok-E burn 2 (LOI simulation)  259.80 177 x 14041 x 51.72 
1970 Nov 28   Simulated passive rendezvous phase 
1970 Dec 5  End of transmissions 
1970 Dec 21   
94.1 179 x 766 x 51.6 
1983 Sep 21   Reentered over 51S, 22W 

Kosmos 704

  1975-005A


A TF beacon was identified during reentry. A pair of debris objects cataloged after launch may have been sensor covers or tracking errors.


Kosmos-704 
 

DateTimeEventOrbit  

1975 Jan 23  1100 Launch by Soyuz-U  Plesetsk 
 1104 Blok-I burn 
 1108 Blok-I sep 
1975 Jan 23    89.57 200 x 305 x 72.9 
1975 Jan 26    89.57 203 x 302 x 72.9 
1975 Jan 27   Lower perigee89.21 166 x 304 x 72.9 
1975 Jan 28    89.16 169 x 296 x 72.9 
1975 Jan 28   Lower apogee88.86 166 x 269 x 72.8 
1975 Jan 29    88.83 166 x 267 x 72.8 
1975 Jan 29   Raise apogee89.56 166 x 339 x 72.9 
1975 Jan 31    89.53 166 x 335 x 72.8 
1975 Feb 1   Raise apogee89.63 167 x 344 x 72.9 
1975 Feb 2   Engine ejected
1975 Feb 5    89.54 167 x 335 x 72.8 
1975 Feb 6   
 0427? Deorbit 
 0437? PO sep 
 0441? Entry 
 0457? Landed 

Falcon Gold

 1997-065B


The 15 kg Falcon Gold payload was built by cadets at the AF Academy, Colorado Springs. It remained attached to the AC-131 Centaur stage. Falcon Gold measures GPS signal strength at geostationary altitudes.

The experiment was a box-shaped device powered by batteries. It was activated 8000s after launch, when the primary DSCS payload was at a safe distance from Centaur.


Falcon Gold 
 

DateTimeEventOrbit  

1997 Oct 25  0046  Launch by Atlas IIA Centaur AC-131 CC SLC36A 
 0048? T+2:44? Atlas BECO 
 0048? T+2:47? Atlas BECO 
  T+3:53? Fairing 
  T+4:41? Atlas SECO 
 0050? T+4:43? Atlas sep 
 0051? T+5:00? Centaur MES-1 
 0056? T+10:07? Centaur MECO-1  150? x 900? x 29?  
 0108? T+22:17? Centaur MES-2 
 0109? T+23:43? Centaur MECO-2 
 0112  T+26:38 Centaur sep from DSCS/IABS 619.1 316 x 35771 x 25.3 (UN) 
 0259  T+2:13:20? FG activated  
1997 Oct 28  622.3 241 x 35294 x 26.4 (UN) 
1997 Nov 5  181 x 35202 x 26.30 (Falcon Gold) 
1997 Nov 9  0245  end of transmissions 

Kosmos 2346

 1997-052A


Kosmos-2346 carried the Faisat-2V satellite to orbit. In plane 1, it may have been a Tsikada-M-UTTH test flight.


Kosmos-2346 
 

DateTimeEventOrbit  

1997 Sep 23  1644:51  Launch by Kosmos-3M  PL 
 1647:01  T+2:10 Stage 1 MECO 
 1647:02  T+2:11 Stage 1 sep 
 1647:05  T+2:14 Stage 2 burn 
 1647:17  T+2:26 Fairing sep 
 1652:56  T+8:05 Stage 2 MECO, low thrust 
 1732:51  T+48:00 Stage 2 burn 2 
 1732:56  T+48:05 Stage 2 MECO 
 1733:16  T+48:25 Stage 2 sep 
 2204:07  Faisat sep from Kosmos-2346 

Aviation Week: August 4,1997

 https://welib.org/md5/9e87fcf93faa8d5034a086a2d6668018

Wednesday, January 21, 1998

The Hollywood Handbook

https://welib.org/md5/cb9d8879c0a0ae8dbe85747250f30218

Kosmos 200

  1968-006A


The first Tselina-O payload was launched in Jan 1968 and became Kosmos-200. The satellite remained in orbit until Feb 1972, when it reentered over the United States 120 km SE of Memphis.


Kosmos-200 
 

DateTimeEventOrbit  

1968 Jan 19 2200:00  Launch by 11K65M  PL 
 2202  Stage 2 burn 
 2208 Stage 2 coast 
 2233? Stage 2 burn 2 
 2233? Stage 2 sep  95.23 523 x 537 x 74.03 (RAE) 
1972 Feb 24   Reentered  

Tuesday, January 20, 1998

Chinasat 1

 1988-014A




The STTW 2 (Zhongxing 1) satellite was launched on 1988 Mar 7 by Chang Zheng 3 from Xichang. It was the first DFH-2A class satellite and went to the 87.5E Chinasat 1 position.


Chinasat 1
 

DateTimeEventOrbit  

1988 Mar 7  1241  Launch by CZ3  XSC 
  T+2:06 St 1 MECO 
  T+2:07 St 2 burn 
  T+4:15 St 2 MECO 
  T+4:19 Fairing 
  T+4:22 St 2 VECO 
  T+4:23 Stage 3 burn 
 1252? T+11:08 MECO-1 
 1300?  Stage 3 MES-2 
 1305? Stage 3 MECO  
 1306? Stage 3 sep 630.26 179 x 35765 x 31.2 
1988 Mar 9  0148  AKM burn  1455.0 35715 x 36597 x 0.5 GEO 124E-5/d 
1988 Mar 10    1457.16 35784 x 36611 x 0.5 GEO 141.5E+5.2W 
1988 Mar 22   mv in  1436.10 35782 x 35791 x 0.2 GEO 87.3E 
1988 Mar 23    GEO 88E 
1988 Apr 3   On station  GEO 87.5E 
1988 Apr 7    1436.07 35767 x 35805 x 0.0 GEO 87.6E 
1989 Jun 24    1436.19 35783 x 35793 x 0.1 GEO 87.2E 
1991 May 19    1436.13 35779 x 35795 x 0.0 GEO 87.5E 
1993 Feb 20    1436.09 35781 x 35791 x 0.0 GEO 87.5E 
1995 Jan 27    1436.06 35776 x 35795 x 1.5 GEO 87.5E 
1996 Apr 9    1436.13 35782 x 35792 x 2.4 GEO 87.9E 

Apollo 13

 https://welib.org/md5/9dd12c3fec9fa04931b2e0f7ce255818

Monday, January 19, 1998

Hexagon 15

 1979-025A


This flight carried the NAVPAC autonomous navigation experiment.


HEXAGON 15 
 

DateTimeEventOrbit  

1979 Mar 16  1830  Launch by Titan IIID  V SLC4E 
  T+1:49? Stage 1 burn 2:27 
  T+1:55 SRM burnout  
  T+1:55 SRM sep 
  T+4:16 Stage 1 MECO 
  T+4:16 Stage 1 sep 
  T+4:16 Stage 2 burn 
  T+5:05? Fairing 
 1837? T+7:44? Stage 2 MECO 
 1838? T+8:00 Stage 2 sep 
   88.6 161 x 247 x 96.4 
1979 Mar 17    156 x 243 x 96.4 
1979 Mar 17    161 x 256 x 96.4 
1979 Mar    160 to 170 x 244 to 260 x 96.4 
1979 Mar 30    167 x 279 x 96.4 
1979 Mar 31    168 x 259 x 96.4 
1979 Apr 1-18    160 to 170 x 240 to 262 x 96.4 
1979 Apr 23    88.56 163 x 242 x 96.4 
1979 Apr 24    88.85 171 x 263 x 96.4 
1979 Apr 26  2044? SRV-1 MAR 
1979 Apr 30  2322   88.73 166 x 257 x 96.35  

1979 Jun 1  

  88.81 164 x 266 x 96.4 
1979 Jun 7   Map op 387 
1979 Jun 8  op 400 
1979 Jun 10  1855   88.61 160 x 251 x 96.3 

1979 Jun 16  

2029? SRV-2 MAR 
1979 Jun 22   op 450 
1979 Jun 30    88.8 167 x 266 x 96.2 (SSR) 
1979 Jul 1   op 475 
1979 Jul 5    88.59 159 x 249 x 96.2 
1979 Jul 7   op 483 
1979 Jul 10   op 486 
1979 Jul 11   op 487 last mapping image 
1979 Jul 12  2033? SRV-5 deorbit opp 
 2105? SRV 1215-5 recovered after 118d 
1979 Jul 15    88.68 162 x 256 x 96.3 
1979 Jul 31  2040? SRV-3 MAR 
1979 Aug 1    88.83 172 x 260 x 96.3 
1979 Aug 15  0623   88.60 161 x248 x 96.3  

1979 Aug 31  

  88.7 165 x 265 x 96.2 (SSR) 
1979 Sep 1    88.65 161 x 254 x 96.2 
1979 Sep 19  2043? SRV-4 MAR 
1979 Sep 201316  88.66 164 x 252 x 96.2 
1979 Sep 22  2115? Reentered after 190d 

May 13,2026

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