Friday, July 30, 2004

USA-173

 2003-054A


A new ocean surveillance SIGINT was launched in Dec 2003 on MLV-14. The Centaur IIA has two RL10A-4-1B engines. The unclassified launch name was Libra. Two satellites were deployed, rather than the expected three, confirming the new Atlas-launched system was a different design to its predecessors.

The satellites each made a stationkeeping burn to join the operational constellation on 2004 Mar 24.


NRO 
 

DateTimeEventOrbit  

2003 Dec 2  1004  Launch by Atlas IIAS AC-164 V SLC3E 
  T+0:57 SRB 3-4 on 
  T+1:59 SRB 1-2 sep 
  T+2:02 SRB 3-4 sep 
  T+2:43 BECO 
  T+2:47 Booster sep
  T+3:29 Fairing sep
  T+4:33 SECO 
  T+4:35 Atlas sep  -5558 x 200 x 63.7 
  T+4:52 MES1 
 1014 T+10:36 MECO1  166 x 1209 x 61.1 
  T+1:10:05 MES2 17s 
 1114 T+1:10:22 MECO2  1008 x 1208 x 63.4 
 1118 T+1:14:05 Centaur sep  1005 x 1218 x 63.5 (UN) 
  ? Payload 2 separates 
2004 Mar 23    107.415 1016 x 1197 x 63.4 
2004 Mar 24   Stationkeeping burn 
2004 Mar 24    107.426 1016 x 1198 x 63.4

Sunday, July 25, 2004

Resourcesat 1

 2003-046A


IRS-P6, or Resourcesat-1, was launched on PSLV in 2003. It replaces IRS-1C and IRS-1D, carrying three improved cameras and a solid state recorder.

The PSLV-C5 launch switched the PSOM burn sequence to four ground lit and two air lit instead of the other way around.

Mass 1360 kg.

\impha{2.5}{90}
  • images/03046A


Resourcesat 
 

DateTimeEventOrbit  

2003 Oct 17  0452 Launch by PSLV-C5   
  T+0:25 Air PSOM 5-6 on  
  T+1:08 Ground PSOM 1-4 sep 
  T+1:30 Air PSOM sep 
  T+1:52 PS1 sep 
  T+1:53 PS2 on 
  T+2:37 Fairing sep at 118 km 
  T+4:25 PS2 sep 
  T+4:27 PS3 on 
  T+6:29 PS3 sep 426 km 
  T+9:00 PS4 MES, 621 km 
 0509 T+17:23 PS4 MECO 
 0510 T+18:00 PS4 sep 
2003 Oct 18    101.69 802 x 875 x 98.7  

Payload:

  • LISS-3 Medium res VNIR/SWIR Multispectral camera, 4 bands; 140 km swath, 23m res

  • LISS-4, High res VNIR camera, 70 km swath, 6m res; 3 bands

  • AWIFS-A/B Advanced Wide Field Sensor VNIR/SWIR 740 km swath, 56m res.

Wednesday, July 21, 2004

Progress M1-11

 2004-002A


11F615A55 No 260. was prepared for launch aboard Soyuz No. 683 (11A511U No. D15000-683) for mission 13P. It carried 2345 kg of cargo including 570 kg? of prop. Launch mass 7230 kg (NK: or 7283 kg).

The spacecraft will be used for ten days of attitude control tests, preparing for future microgravity experiment missions.

Matroshka  [457] is a dummy human torso to be installed on the SM exterior. Launch by Progress 260; to be retrieved with return on Soyuz. Other ESA experiments for DELTA were carried.

On departure, with a mass of 5703 kg, it carried Orlan-M no 1280023.


Progress 260 
 

DateTimeEventOrbit  

2004 Jan 29  1158:08 Launch by Soyuz-U  KB PL1/5 
  T+1:59 Strapons 
  T+2:43 GO sep 
  T+4:45 Blok A MECO 
  T+4:47 Blok A sep 
  T+4:57 KhO sep 
 1206:54 T+8:46 Blok I MECO 
 1206:57 T+8:49 Blok I sep  88.62 178 x 234 x 51.7 
 1533:16  DV1 30s 11.4m/s 
 1610:51 DV2 16.7s 6.2m/s  89.23 218 x 254 x 51.6  
2004 Jan 30  1248:16 DV3 2m/s 6.3s 
2004 Jan 31  1108s DV4 
 1248s  Flyaround 
 1257s  Stationkeeping 
2004 Jan 31  1313:11 Docked Zvezda 
2004 May 24  0919:29  Undocked 
 0922? U+3min DPO burn 15s 
 1216:40  DU 23.74s 12.1 m/s  
2004 Jun 3  0950:00  Deorbit 150.3s 79.4m/s 
 1025:01  Entry interface 
 1030:15 70 km

Tuesday, July 20, 2004

Kosmos 2394

 2002-060A


Glonass Bloc 31 launch with Uragan 11F654 792/791/793 to be placed in slots 21, 22 23 of orbit plane 3. Mass 1450 kg each.

Spacecraft 791 entered service on 2003 Feb 10.


Kosmos-2394/Uragan 791 
 

DateTimeEventOrbit  

2002 Dec 25 0737:58  Launch by Proton  PL 81/23 
 0740:05  T+2:07 St 1 sep 
 0741:16  GO sep 
 0743:36  St 2 sep 
 0747:38  T+9:40 St 3 MECO 
 0747:50  T+9:52 St 3 sep  162 x 185 x 64.9 
 0748:45  Adapter sep 
 0834:57  SOZ-1 
 0839:56  MES-1 
 0845:49  MECO-1  196 x 19137 x 64.6 
 1127:47  SOZ-2 
 1132:47  MES-2 
 1132:47  SOZ-2 cutoff 
 1135:11  MECO-2 
 1135:25  DM sep KA-1 
 1153  KA-2 sep? 
 1211  KA-3 sep? 

Sunday, July 18, 2004

Aviation Week: February 2,2004

 https://welib.org/md5/b4b562e14cf2fa38793740ea23683118

Kosmos 953

 1977-089A



Kosmos-953 
 

DateTimeEventOrbit  

1977 Sep 16  1430 Launch by Soyuz-U  Plesetsk 
 1434  Blok-I burn 
 1438  Blok-I sep 
1977 Sep 16    89.62 179 x 331 x 62.8 
1977 Sep 18   
89.36 173 x 312 x 62.8 
1977 Sep 21    89.73 172 x 305 x 62.8 
1977 Sep 22   
89.00 150 x 299 x 62.81 
1977 Sep 24    88.81 148 x 282 x 62.8 
1977 Sep 25   
89.52 152 x 351 x 62.8 
1977 Sep 28    89.39 152 x 336 x 62.8 
1977 Sep 30  
 0540?  Deorbit 
 0550?  PO sep 
 0554? Entry 
 0612? Landed 

Tuesday, July 6, 2004

CBERS-2

 2002-049A


The second ZY-2 was launched in Oct 2002 into a similar orbit to the first, and almost the same orbital plane. The orbit was raised to operational height between Nov 6 and 14, after which monthly tweak burns maintained the orbit. In Jan 2003, the satellites were 180 deg apart in their orbit.


ZY-2 No. 2 
 

DateTimeEventOrbit  

2002 Oct 27  0317  Launch by CZ-4B  TYSC 
  T+2:33 Stage 1 MECO 
  T+2:34 Stage 1 sep 
  T+2:54 Fairing sep 
  T+4:37 St 2 MECO 
  T+4:47 St 2 VECO 
  T+4:48 St 2 sep 
  T+4:48 St 3 burn 
 0328 T+11:18 St 3 MECO 
 0329 T+12:28 ZY 2 sep  
 0335? St 3 passivation  396 x 575 x 97.3  
2002 Oct 27    94.14 470 x 483 x 97.4 
2002 Nov 6   Orbit raise  94.20 472 x 486 x 97.4 
2002 Nov 8   Orbit raise  94.40 475 x 504 x 97.4 
2002 Nov 14   Orbit raise  94.45 477 x 506 x 97.4 
2002 Dec 5    94.41 476 x 503 x 97.4 
2002 Dec 7   Orbit trim  94.45 480 x 503 x 97.4 
2002 Dec 26    94.41 479 x 500 x 97.4 
2002 Dec 28   Orbit trim 94.45 482 x 501 x 97.4 
2003 Jan 22    94.42 481 x 499 x 97.4 
2003 Jan 23   Orbit trim 94.45 483 x 500 x 97.4 
2003 Feb 21    94.42 480 x 499 x 97.4 
2003 Feb 23   Orbit trim  94.45 483 x 500 x 97.4 
2003 Mar 19    94.42 482 x 498 x 97.4 
2003 Mar 23   Orbit trim 94.45 485 x 498 x 97.4 
2003 Apr 13    94.42 485 x 496 x 97.4 
2003 Apr 19   Orbit trim  94.46 487 x 497 x 97.4 
2003 May 26    94.41 483 x 497 x 97.4 
2003 May 29   Orbit trim  94.45 485 x 497 x 97.4 
2003 Jul 6    94.42 484 x 496 x 97.4 
2003 Jul 13   Orbit trim  94.44 486 x 496 x 97.4 
2003 Aug 23   Orbit trim 
2003 Sep 28    94.42 484 x 495 x 97.37 
2003 Oct 5   Orbit trim  94.44 487 x 495 x 97.37 
2003 Nov 7    94.40 487 x 492 x 97.36 
2003 Nov 13   Orbit trim 94.44 487 x 495 x 97.36 
2003 Dec 7    94.42 485 x 495 x 97.36 
2003 Dec 9   Orbit trim  94.45 487 x 495 x 97.36 
2004 Jan 18    94.42 485 x 496 x 97.35 
2004 Jan 20   Orbit trim 94.44 487 x 496 x 97.35 
2004 Feb 15    94.43 487 x 494 x 97.35 

Sunday, July 4, 2004

Galaxy 5

 1992-013A


The HS376 Galaxy V was used as a video relay station for cable TV distribution. It was owned by Hughes Communications Inc.


Galaxy 5 
 

DateTimeEventOrbit  

1992 Mar 14  0016Launch by Atlas I Centaur   
  T+2:34 BECO 
  T+2:37 Booster sep 
  T+3:00 Insulation panels sep 
  T+3:34 SECO, VECO 
  T+3:36 Atlas sep 
  T+4:48 MES1 
  T+9:52 Perigee positive  
  T+10:09 MECO1  148 x 2252 x 28.5 
  T+25:39 MES2 
  T+27:06 MECO2  1120 x 36132 x 19.7 
  T+29:32 Centaur sep  
  Centaur vent  1107 x 35254 x 19.7 (B) 
1992 Mar 13    656.26 1122 x 36152 x 19.3 
1992 Mar 16    655.81 1120 x 36131 x 19.7 
1992 Mar 17  2116?  Star 30C AKM fired  34564 x 35891 x 0.3 
1992 Mar 17    1409.21 34600 x 35916 x 0.3  
1992 Mar 22    1436.39 35708 x 35876 x 0.2 GEO 134.9W+0.08W 
1992 Mar 29    1436.09 35693 x 35880 x 0.1 GEO 135.0W 
1992 Apr 6   mv out  1434.24 35692 x 35808 x 0.1 GEO 132.8W+0.4E 
1992 May 20    1436.07 35777 x 35794 x 0.1 GEO 125.0W 
1993 Mar 1    1436.07 35785 x 35786 x 0.0 GEO 125.1W 
1994 May 26    1436.02 35780 x 35789 x 0.0 GEO 124.9W 
1995 May 4    1436.08 35781 x 35790 x 0.0 GEO 125.0W 
1997 May 16   To Panamsat  GEO 125W 
1999 Jun 14    1436.04 35777 x 35793 x 0.1 GEO 125.0W 
2004 Jan 18    1436.08 35781 x 35790 x 0.1 GEO 125.2

Man in Space: An Illustrated History from Sputnik to Columbia

 https://welib.org/md5/ac8dec49ea58c5989447d3f20dbd3803

Saturday, July 3, 2004

Progress M1-4

 2000-073A


Progress M1-4 was launched to Zarya's nadir port. A software problem with the Kurs system sent Progress into oscillations at a range of 100m. Gidzenko took TORU control but the camera iced up; he backed it off until the picture improved and then came back in for a successful manual remote docking.

The Progress was quickly unloaded and then undocked prior to the STS-97 approach on Dec 1. Loaded with improved software, the craft made a flawless second approach on Dec 26. The Kurs close-approach antenna had been irreversibly retracted on the initial docking, so the final approach had to be done with TORU again. Gidzenko took TORU control and brought the craft in to a docking, once again at the Zarya nadir.

Launch mass was 7285 kg. It carried 874 kg of propellant (760 kg in OKD and 114 kg in GO or PAO?). GO cargo was 1358 kg, assume 1244 kg of it was dry. 


Progress M1-4 
 

DateTimeEventOrbit  

2000 Nov 16 0132:36  Launch by Soyuz-U 
 0141:25  Blok I sep 
 0507:22  TCM1 20m/s 52s 
 0545:32  TCM2 11 m/s 42s 
2000 Nov 17  0237:23  TCM3 0.9m/s 3s 
2000 Nov 18  0058:37  SKD 59m/s 22s 
 0120:57  DPO 30m/s 1s 
 0144:35  SKD 87m/s 35s 
 0228:07  SKD 20 m/s 6s 
 0234:29 SKD 18m/s 4s 
 0236:19  DPO 28m/s 1.5s 
 0239  Begin flyaround 
 0251  Skeep 200m 
 0259  Range 150m 
 0302  Range 100m 
 0302  Gidzenko takes manual control 
  TORU approach 
 0309  Range 5 m, skeep 
 0322? Back off to 35m, skeep 
  TORU approach 
 0347:42  Docked at -Y(FGB) 
2000 Dec 1  1623  Undocked from Zarya nadir 
 1627  Sep burn 
2000 Dec 20  1255  Rendezvous burn (range 2200 km) 
2000 Dec 24 Rendezvous burn 
2000 Dec 26   Approach ISS 
 1015  At 3.7 km 
 1020  At 900m 
 1027  Rendezvous, Begin flyaround at 240m 
 1038  Stationkeeping at 190m 
 1052  Switch from Zvezda to Zarya antenna 
  Aligned with Zarya 
 1054 Gidzenko takes TORU control at 200m 
 1103  Dock with Zarya nadir 
2001 Feb 8  1126:04  Undock from Zarya nadir 

1318Deorbited 
 1350  Reentered over Pacific 

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