Monday, September 8, 1997

ESSA 5

  1967-036A


ESSA V was another global weather monitoring satellite with an AVCS camera system. Launched from Vandenberg on 1967 Apr 20, it entered a 1361 x 1423 km x 102.0 deg orbit and replaced ESSA III. It transmitted until 1970 Feb 20.


ESSA 5 
 

DateTimeEventOrbit  

1967 Apr 20  1121:10  Launch by Delta E  V SLC2E 
  T+0:43 SRM out 
  T+1:10 SRM sep 
 1123:42  T+2:32 Thor S/N 20215 MECO 
  T+2:34 Thor sep 
 1123  T+2:34 Delta S/N 20214 burn 6:11 
  T+2:38 Fairing sep 
 1129:59 T+8:49 Delta SECO V=5.87 km/s 
 1139:33 T+18:23 X-258C4 RH141 burn 23s 
 1139:56 T+18:46 X-258 burnout  1361 x 1423 x 102.0  
 1141:18 T+20:08 X-258 sep 
1967 Apr 24   Cameras on 
1967 May 8   To ESSA,replaced ESSA 3 
1970 Feb 20   end of tx 

Saturday, September 6, 1997

Progress M-4

 1990-072A


Progress M 11F615A55 No. 204 (Progress M-4) was launched in Aug 1990. It docked with Mir on Aug 17 delivering 2689 kg of cargo. After undocking on Sep 18 it carried out the Fokus plasma gun experiment injecting plasma into the ionosphere. One debris object was cataloged prior to reentry, possibly related to Fokus. 


Progress M-4 
 

DateTimeEventOrbit  

1990 Aug 15  0400:38Launch by Soyuz-U  KB 
 0405  Blok-I burn 
 0409  Blok-I sep 
 0840 88.52 183 x 219 x 51.61 
 1200   89.70 249 x 269 x 51.60 
1990 Aug 16  0700   89.73 250 x 271 x 51.61 
1990 Aug 17  0230 89.71 249 x 270 x 51.61 
 0526:18Docked with Mir DP1 
1990 Aug 18  1000 92.03 367 x 380 x 51.61 
1990 Sep 17  1242:43  Undocked 
1990 Sep 18  0500 92.37 373 x 407 x 51.61 
 0620Fokus plasma source release 
1990 Sep 19  1730Object 72C tracked 
1990 Sep 20  1105Retrofire
 1142:49  Reentered over Pacific 

Kosmos 1008

 1978-049A


This was the third Tselina-OK satellite.


Kosmos-1008 
 

DateTimeEventOrbit  

1978 May 17 1439  Launch by 11K65M  Plesetsk 
 1441  S3 burn 
 1447? T+8m? S3 MECO-1 
 1512? T+33m? S3 MES-2 
 1512? S3 sep 
1978 May 17   95.1 499x549x74.0 
1981 Jan 8   reentered 

Friday, September 5, 1997

Meteor-1 18

  1974-052A


Meteor 11F614M No. 24 was launched on 1974 Jul 9. It was a prototype of the new Meteor-Priroda series. The satellite was later given the designation Meteor-Priroda 11F651 No. 1. It was the second mission to carry a low thrust plasma engine. 


Meteor-Priroda No. 1 
 

DateTimeEventOrbit  

1974 Jul 9  1440 Launch by Vostok 8A92M  PL 
 1444? Blok E burn 
 1450? Blok E sep 
   102.6 865 x 893 x 81.2 
1975 Nov    103.1 890 x 918 x 81.2 
1976 Oct 28   end of ops 

Kosmos 305

  1969-092


Kosmos-305 (E-8-5 No. 404) suffered the same fate as Kosmos-300 in the following month's launch window. Various reports claimed that the Blok-D disintegrated or that the payload may have entered a high orbit, but the modern consensus seems to be that the second burn was cut short and occurred at the wrong orientation, with rapid reentry of the payload and Blok-D.


Kosmos-305 
 

DateTimeEventOrbit  

1969 Oct 22  1409:59  Launch by Proton-K  KB LC81 
 1412?  Stage 2 burn 
 1415?Stage 3 burn 
 1419  Stage 3 sep  -800? x 210 x 51.5 
 1425?  Blok-D burn 1  
 1427?  Blok-D cutoff 1, parking orbit  182 x 210 x 51.5? 
 1436?  Stage 3 reentry 
 1520?  Blok-D burn 2  
 1520?  SOZ burn 
 1520? SOZ sep (92A/B) 
 1530?  Blok-D MECO?  70? x 187? x 51.5 
 1615  Reentry over Australia? 

Monday, September 1, 1997

IRS-1A

 1988-021A


IRS-1A took off from Baikonur aboard a Vostok 8A92M on a southbond trajectory to polar sun-synchronous orbit.


IRS-1A 
 

DateTimeEventOrbit  

1988 Mar 17  0643:30  Launch by Vostok 8A92M  KB LC31  
 0645:30  Blok-BVGD sep (T+2:00) 
 0646:30  Fairing sep (T+3:00), 160 km 
 0648:40  Blok-A cutoff, Blok-E burn (T+5:10) 
 0654:30  Blok-E cutoff (T+11:00) 
 0654:40  Payload release (T+11:10) 
   102.82 870 x 914 x 99.0 
1988 Apr 7   Complete orbit maneuvers 
1991   Still operating 
1995 Mar 17   On standby status 

Payload:

  • Radiometers

  • LISS cameras - linear imaging self scanning CCD

  • LISS 1: 72m res, 148 km swath, 4000-9000A in 4 bands

  • LISS 2: 36m res, 74 km swath, 4000-9000A in 4 bands

Tuesday, August 26, 1997

Soyuz 15 (Danube)

 1974-067A


11F615A9 No. 63 (Soyuz-15) was launched on 1974 Aug 26, the second flight to Almaz OPS 2. The spacecraft made rendezvous with the space station the next day, but the docking was aborted. At 350 m range, the Igla system decided the range was actually 20 km and increased approach speed to 20 m/s - Soyuz rushed past the station, missing it by only 40 m. The automatic system repeated this close flyby twice more. Ground control shut down the system and the mission was returned early.


Soyuz-15 
 

DateTimeEventOrbit  

1974 Aug 26  1958:05  Launch by Soyuz  KB 
 2000 Blok BVGD sep 
 2004  Blok A sep 
 2006  Blok I MECO 
 2006  Blok-I sep 
   195 x 221 x 51.6 
  Orbit raise  254 x 275 x 51.6 
1974 Aug 27  1900?  Rendezvous with Salyut-3 
  Flyby 1 at 40 m 
  Flyby 2 at circa 40 m 
  Flyby 3 at circa 40m 
  Failed to dock 
1974 Aug 28  1924  Retrofire  258 x 278x 51.6 
 1927?  DO CO   
 1940?  Modules sep 
 1946?  Entry  -103? x 258 x 51.6 
 2010:16  Landed 48 km SW of Tselinograd

Wednesday, August 20, 1997

Kosmos 2001

 1989-011A



Kosmos-2001 
 

DateTimeEventOrbit  

1989 Feb 14  0421:11 Launch by 8K78M  Plesetsk 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 0430 T+8:50 Blok-I sep 
  T+1:00? BOZ burn 
 0521?  T+1:00? BOZ sep 
  2BL burn 
  2BL MECO 
 0524?  T+1:03 2BL sep  
1989 Feb 14   92.67 211x600x62.8 
1989 Feb 15  708.5 617x39279x62.8

STS-60 (Discovery)

 1994-006A


STS-60 was launched on 1994 Feb 3 at 1210 on a research mission to fly the Wake Shield Facility and carry out research in the Spacehab module on materials and bioprocessing. The original plan was to release the WSF into a 350 x 354 km orbit at 1400 on Feb 5, and rendezvous with it on Feb 7, retrieving it at 2010. However, problems with WSF attitude control aborted the deploy on two occasions, and it was used instead attached to the RMS arm.

The CAPL experiment showed that start-up of the capillary pumped loop thermal control system was much harder in orbit than on the ground, prompting a redesign of the system.

Six ODERACS calibration spheres and the German BREMSAT microsat were ejected from the GAS bridge during the mission.


STS-60 events 
 

DateTimeEventOrbit  

1994 Jan 4   Tow to VAB 
1994 Jan 10   Rollout  LC39A 
1994 Feb 3  1210:00  Launch from LC39 
 1212:05  SRB sep 
 1218:33 MECO  88.74 66 x 357 x 57.0 (OMS dV) 
 1218:52  ET sep 
 1252:16  OMS-2 2:44 82m/s 
 1255:00  OMS 2 CO 91.60 347 x 358 x 57.0 
 1341  PLBD open 
1994 Feb 4  0000   91.59 347 x 358 x 57.0 
  RMS tests 
1994 Feb 5  0944  Supply water dump 

1113:57  RMS grapple WSF 
 1223:41  WSF unberth 
  WSF deploy cancelled 
 2058  RMS reberth WSF 
 2103  Ungrapple 
1994 Feb 6  1114  RMS grapple WSF 
 1153 RMS unberth WSF 
1994 Feb 7  1721  RMS reberth WSF  91.58 345 x 358 x 57.0 
 1724  Ungrapple 
 1724  Grapple 
 2051  Unberth 
1994 Feb 8  1159  Berth 
 1434  Unberth 
1994 Feb 9  0657   91.58 345 x 358 x 57.0 
 1218  Berth 
 1245  Ungrapple WSF 
 1453:24  ODERACS deploy sequence initiated 

1454:23  ODERACS-A (10cm) deploy 
 1454:25  ODERACS B (10cm) deploy 
 1454:28  ODERACS C (5 cm) deploy 
 1454:30  ODERACS D (5 cm) deploy 
 1454:35  ODERACS E (15cm) deploy 
 1454:37  ODERACS F (15cm) deploy 
 1923:19  BREMSAT deploy 
1994 Feb 10  0700   91.62 349 x 358 x 57.0 
1994 Feb 11  1409  PLBD closed  91.63 349 x 358 x 57.0 
 1814:50  OMS DO (3:54) 124m/s  
 1818:45  OMS DO CO  87.39 -67 x 358 x 57.0 
 1847:51  Entry interface 
 1919:22  Landed KSC RW15 
 1919:35  Chute 
 1919:43  NGTD 
 1919:57  Chute sep 
 1920:14  Wheels stop 
 2245Tow to OPF/3 

Friday, August 15, 1997

Morelos 1

 1985-048B


The Morelos 1 satellite was owned by Mexico's Secretaria de Comunicaciones y Transportes (SCT). The satellite was deployed with its PAM-D upper stage from Space Shuttle Discovery in Jun 1985.


Morelos 1 
 

DateTimeEventOrbit  

1985 Jun 17  1938  Deploy  
 2023  PAM-D burn 
 2024  PAM-D cutoff 
 2026  PAM-D sep 
1985 Jun 17    635.90 375 x 35859 x 25.4 
1985 Jun 18    645.76 818 x 35921 x 23.3 
1985 Jun 18  2316 Star 30BP burn 
   1315.71 30860 x 35932 x 0.0 GEO 172.7W+33.0E 
1985 Jun 20   lower orbit 1432.79 35499 x 35943 x 0.2 GEO 112.9W+0.8E 
1985 Jun 21    1436.38 35782 x 35801 x 0.1 GEO 113.3W+0.08W 
1985 Jun 29    1436.10 35779 x 35793 x 0.1 GEO 113.5W+0.0W 
1986 Oct 1    1436.07 35776 x 35796 x 0.0 GEO 113.4W+0.0W 
1989 Jan 30    1436.08 35776 x 35796 x 0.0 GEO 113.6W 
1990 May 13    1436.07 35769 x 35802 x 0.0 GEO 113.4W 
1992 Jun 13    1436.09 35776 x 35796 x 0.0 GEO 113.5W 
1994 Feb 27    1436.06 35779 x 35792 x 0.1 GEO 113.4W 

Sunset Fling

https://welib.org/md5/5c3097041b6da97f7dd25b87b951f072

Sunday, August 10, 1997

Crystal 6

 1984-122A


CRYSTAL 6 was launched into a late afternoon 0941 LTDN west-plane sun-synchronous orbit. The higher apogee of this mission reflected the KENNEN system's takeover of the HEXAGON's wide area search mission in addition to the core KH-11 close-look capability. D. Day notes that the search mission is performed at apogee and in a sun-synchronous orbit the orbital plane would be 180 degrees from a high resolution mission looking at the same target at perigee.


CRYSTAL 6 
 

DateTimeEventOrbit  

1984 Dec 4 1803 Launch by Titan 34D  V SLC4E 
 1804  Core engines on (T+1:47) 
 1804  SRM jettison (T+1:56) at 39 km  
 1807?  T+4min? Stage 1 sep  
 1807?  Stage 2 ignition (T+4:33?) 
 1807?  Fairing off (T+4:46?) 
 1810?  Stage 2 cutoff (T+7:58?) 
 1811?  Stage 2 sep (T+8:08?)   
1984 Dec 4   93.5 300x650x97.1 
1989 May 6   96.55 302x884x97.8 
1989 Aug 1   96.08 298x843x97.8 
1989 Aug 14   96.53 352x832x97.9 
1989 Aug 18   96.51 349x834x97.8 
1989 Aug 22   96.50 345x837x97.8 
1990 Mar 31   95.78 376x736x97.63 (Molczan CSS1731) 
1990 Apr 2   95.81 340x775x97.8 
1990 Jun 3    95.60 336x758x97.7 (CSS2333) 
1990 Oct 9    336x732x97.8 
1990 Nov 12   
559x732 from 336x732 
1991 May 25    97.51 552x726x97.8 (CSS) 
1991 Jul 9    97.23 541x711x97.8 (CSS) 
1992 Oct 7    97.39 561 x 705 x 97.8 
1993 Jul 14    97.36 542 x 722 x 97.8 
1994 Oct 13    97.34 544 x 718 x 97.9 
1996 Feb 22 Reentered 

Kosmos 1875

 1987-074A


Kosmos-1875 was the first satellite of the fourth Strela-3 launch.


Kosmos-1875 
 

DateTimeEventOrbit  

1987 Sep 7  2350:09 Launch by Tsiklon-3  PL 
  T+2:00 St 1 sep 
  T+3:33 GO sep 
  T+4:38 St 2 sep 
  T+6:00 S5M burn 1 96s 
 2357  T+7:36 S5M MECO-1-200? x 1300 x 82.6 
1987 Sep 8  0032?  T+41:50 S5M burn 2 25s 
  T+42:10 S5M low thrust 
  T+42:43 S5M sep first KA 
 0034?  T+44:09 S5M sep last KA 
1987 Sep 25   113.72 1372x1423x82.5

November 20,2006

  https://en.wikipedia.org/wiki/Association_football