Tuesday, June 28, 2005
Friday, June 24, 2005
Monday, June 20, 2005
ADEOS-2
2002-056A
ADEOS 2 has a mass of 3680 kg. Size 6 x 4 x 4m, 28 m span, Irreg + 1 panel. GLI will have 36 bands, 1 km res. AMSR has 10 km res at high freq. This was the first launch since MHI took over launch operations from NASDA on Nov 20. Communications with the satellite failed in Oct 2003, almost exactly the same interval after launch as the ADEOS-1 failure.
| ADEOS-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2002 Dec 14 | 0131 | Launch by H-2A | |
| T+1:40 SRB-A burnout | |||
| T+1:47 SRB-A sep | |||
| T+4:20 5S PLF sep | |||
| T+6:35 St 1 MECO | |||
| T+6:43 St 1 sep | |||
| 0137 | T+6:49 St 2 MES | -5600? x 500? | |
| 0146 | T+15:38 St 2 MECO | ||
| 0147 | T+16:28 ADEOS sep | 804 x 806 x 98.7 | |
| 0201 | T+30:55 Fedsat sep | ||
| 0203 | T+32:40 WEOS sep | ||
| 0205 | T+34:30 MuLabSat sep | ||
| 2002 Dec 17 | Intersat comms antenna deploy | ||
| 2003 Oct 24 | In safemode | ||
| 2300 | Power and comms unstable, LOS | ||
Payload:
- AMSR Adv Microwave scanning radiometer 6.9-53 GHz
- GLI Global Imager; Ocean, land and cloud, 3750A-12.5mu
- IOCS Inter-orbit comms system
- SeaWinds Wind speed sensor.
- CCR Corner cube reflector
- DCS Data collection system
- POLDER Polarization and Directionality of Earth Reflectance
- VMS ODV-4 visual monitoring system (TV camera to observe solar paddle)
STS-100 (Endeavour)
2001-016A
STS-100 carried out mission 6A, delivering the SSRMS arm Canadarm-2. Press kit quotes Launch mass was 103504 kg; landing mass was to be 99740 kg. However, mass post NC2 burn was almost 114000 kg. Deorbit mass was around 99000 kg.
The mission was extended two days when ISS computer failures delayed the end of SSRMS tests.
| STS-100 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2001 Mar 17 | Tow from OPF/2 to VAB/3 | ||
| 2001 Mar 19 | Mate with ET | ||
| 2001 Mar 22 | Roll to LC39A | ||
| 2001 Apr 19 | 1840:42 | Launch | |
| 1842:46 | SRB sep | ||
| 1842:56 | OMS-1 assist | ||
| 1844:38 | OMS-1 CO | ||
| 1849:08 | MECO | ||
| 1849:27 | ET sep | 74 x 329 x 51.6 | |
| 1924:24 | OMS-2 54s 25m/s | 89.39 159 x 329 x 51.6 | |
| 1925:18 | OMS-2 CO | ||
| 2017:07 | PLBD open | ||
| 2223:19 | OMS-3 NC1 burn 26m/s | 90.23 242 x 328 x 51.6 | |
| 2224:11 | OMS-3 CO | ||
| 2001 Apr 20 | 1042:37 | OMS-4 R NC2 burn | 90.31 247 x 332 x 51.6 |
| 1042:48 | OMS-4 CO | ||
| 2052:12 | OMS-5 NC3 burn 36m/s | 91.61 331 x 375 x 51.6 | |
| 2053:30 | OMS-5 CO | ||
| 2001 Apr 21 | 0900 | 0.1m/s burn | |
| 0944:53 | OMS-6 NC4 burn 13.4m/s | ||
| 0945:21 | OMS-6 CO | ||
| 1117:25 | OMS-7 L TI burn 2.8m/s | ||
| 1117:38 | OMS-7 CO | ||
| 1137:24 | MC1 0.5m/s | ||
| 1214:18 | MC2 0.6m/s | ||
| 1231:18 | MC3 0.2m/s | ||
| 1241:18 | MC4 0.1m/s | ||
| 1256 | On -Rbar at 200m | ||
| 1310 | On Vbar at 94m | ||
| 1324 | Approaching at 70m | ||
| 1328 | At 57m | ||
| 1338 | At 36m | ||
| 1341 | At 30m | ||
| 1347 | At 20m | ||
| 1353 | 10m on final approach | ||
| 1358:49 | Docking at PMA-2 | ||
| 1410:42 | Hard dock | 92.22 375 x 391 x 51.6 | |
| 2001 Apr 22 | |||
| 0810 | RMS uncradle | ||
| 0823:41 | RMS grapple SLP | ||
| 0842 | SLP unberthed | ||
| 1042 | SLP berthed to LCA | ||
| 1117:58 | RMS ungrapple SLP | ||
| EVA-1 Hadfield, Parazynski | |||
| 1131 | Begin depress 9psi | ||
| 1134 | At 5psi | ||
| 1138 | Resume depress | ||
| 1143:02 | Depress complete | ||
| 1144? | HO | ||
| 1145 | Battery power | ||
| 1152 | TC open | ||
| 1152 | Egress EV1 | ||
| 1158 | Egress EV2 | ||
| 1302 | UHF ant unberthed from SLP by Hadfield on RMS | ||
| 1330 | UHF antenna install complete | ||
| 1500 | SSRMS boom raised | ||
| SSRMS bolts fastened | |||
| 1810? | Ingress EV2 | ||
| 1835 | Ingress EV1 | ||
| 1839 | TC closed | ||
| 1845 | HC | ||
| 1855:27 | Repress 7:10:12 (NASA) | ||
| 2005 | RMS recradle | ||
| 2001 Apr 23 | 0930 | HO to ISS | |
| 1114 | SSRMS LEE-B unberthed from SLP | ||
| 1416 | SSRMS LEE-B grapple Destiny PDGF | ||
| 1425:57 | MPLM grappled by RMS | ||
| 1458 | MPLM unberthed from bay | ||
| 1458 | RMS lifting MPLM | ||
| 1600 | Raffaello berthed to Unity -Z | ||
| 1616:03 | MPLM ungrapple | ||
| 1926 | HC to ISS | ||
| 1950:54 | Reboost-1 59:36 2.3m/s | ||
| 2001 Apr 24 | EVA-2 | ||
| 1222 | Begin depress | ||
| 1231:29 | Depress | ||
| 1232? | HO | ||
| 1234 | Battery power | ||
| TC open | |||
| 1240? | Egress | ||
| 1455 | SSRMS power connected | ||
| 1428 | Early COMM antenna removed from Unity | ||
| 1825 | SLP unberth from LCA, on SSRMS LEE-A | ||
| 1905 | DCSU unberth | ||
| 1916 | DCSU berthed to Destiny ESP | ||
| 1950 | EV1 Ingress | ||
| 2000 | EV2 ingress | ||
| 2001? | TC closed | ||
| 2003 | Hatch closed | ||
| 2013:18 | Repress | ||
| 2130? | Hatch open to ISS | ||
| 2001 Apr 25 | Computer problems on ISS | ||
| 2001 Apr 27 | 1120:42 | Reboost-2 60:00 4.8m/s | |
| 1806:38 | RMS grapple MPLM | ||
| 2003 | MPLM unberthed from Unity | ||
| 2059 | MPLM berthed in bay | ||
| 2105:39 | RMS ungrapple MPLM | ||
| 2001 Apr 28 | 2043:42 | RMS grapple SLP | |
| 2056 | SSRMS latches release SLP | ||
| 2102 | SSRMS ungrapple SLP | ||
| 2251 | RMS berth SLP | ||
| 2257:27 | RMS ungrapple SLP | ||
| 2001 Apr 29 | 1620 | Hatches closed to ISS | |
| 1734:04 | Undocking along +Vbar 1m/s | ||
| 1754 | Begin flyaround at 100m | ||
| 1801 | On +Rbar | ||
| 1815 | On -Vbar at 200m | ||
| 1828 | Sep burn on +Rbar | ||
| 2001 May 1 | 1058 | PLBD closed | |
| 1502:47 | OMS DO 3:34 EAFB186 0.111km/s | ||
| 1506:20 | OMS DO cutoff | ||
| 1539:17 | Entry interface | ||
| 1610:43 | Landed on EAFB RW22 11d:21:30:00 | ||
| 1610:53 | NGTD | ||
| 1611:56 | Wheels stop | ||
| 2001 May 8 | 1330 | SCA 905 depart EAFB | |
| 1705 | SCA arrive at Altus AFB OK | ||
| 1915 | SCA depart Altus AFB | ||
| 2022 | SCA arrive at Little Rock AFB | ||
| 2001 May 9 | 1533 | SCA depart Little Rock AFB | |
| 1809 | SCA 905 landed at SLF RW15 | ||
| 2001 May 10 | 0130 | Tow to OPF/1 | |
Friday, June 17, 2005
Navstar 37
1993-032A
Navstar 37 (USA 91) was launched on 1993 May 13. It was stationed at plane C-4 and given the ID PRN 07.
| Navstar 37 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1993 May 13 | 0007:00 | Launch by Delta 7925 | CC LC17 |
| T+0:56 SRM 1-3,7-9 out | |||
| T+1:01 SRM 4-6 on | |||
| T+1:02 SRM 1-3 sep | |||
| T+1:03 SRM 7-9 sep | |||
| T+1:57 SRM 4-6 off | |||
| T+2:02 SRM 4-6 sep | |||
| T+4:25 MECO | |||
| T+4:31 VECO | |||
| T+4:33 Stage 1 sep | |||
| 0011 | Stage 2 TIG (T+4:38) | ||
| 0011 | Fairing sep (T+4:50) | ||
| 0018? | SECO-1 (T+11:37) | 186 x 186? x 34.0? | |
| 0027? | T+20 SES-2 | ||
| 0027? | SECO-2 | 185 x 732? x 34.0 | |
| T+20:55 spinup | |||
| 0028 | T+21 Delta sep | ||
| 0029 | T+22 TES | ||
| 0030 | T+23 TECO | 355.32 171 x 20308 x 37.7 | |
| 0031 | T+24 Stage 3 sep | ||
| 0031 | T+24 Yo weight | ||
| 0113? | SES-3 | ||
| SECO-3 depletion | 96.74 472 x 732 x 21.9 | ||
| 1993 May 14 | 2118? | Star 37XFP burn | 716.92 20048 x 20263 x 55.0 |
| 1993 Jun 12 | In service | ||
| 1993 Aug 22 | 717.93 20026 x 20335 x 55.0 | ||
| 1997 Feb 1 | Operating at slot C-4 | ||
| 2003 Dec 20 | decommissioned | ||
XM-3 (Rhythm)
2005-008A
Launch of XM-3 as backup by Zenit-3SL in 2005. Satellite is a BSS702. It will replace XM1 at 85W, XM1 will move to 115W colocated with XM2, which will be replaced by XM4 in 2007. Accourding to some sources, XM-3 is nicknamed Rhythm.
Launch mass 4703 kg, BOL mass 2950 kg. Size 3 x 3.3 x 7m, with 40.4m span.
| XM3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2005 Mar 1 | 0351 | Launch by Zenit-3SL | |
| T+2:30 St 1 sep | |||
| T+3:46 PLF sep | |||
| 0359 | T+8:31 St 2 sep 176 km | -2009 x 178 x 0 | |
| 0359 | T+8:41 DM MES-1 | ||
| 0408 | T+17:10 MECO-1 207 km | 180 x 9452 x 0 | |
| 0438 | T+47:09 DM MES-2 | ||
| 0441 | T+50:18 MECO-2 | 675.71 2491 x 35767 x 0.1 | |
| 0451 | T+1:00:58 DM sep | ||
| 2005 Mar 1 | 675.71 2491 x 35767 x 0.1 | ||
| 2005 Mar 4 | 739.73 5749 x 35682 x 0.1 | ||
| 2005 Mar 5 | 841.50 5757 x 35760 x 0.5 | ||
| 2005 Mar 7 | 991.67 17390 x 35735 x 0.3 | ||
| 2005 Mar 9 | 1411.47 34824 x 35781 x 0.1 GEO 92.6W+6.3/d | ||
| 2005 Mar 11 | 1431.13 35595 x 35783 x 0.1 GEO 80.1W+1.2E/d | ||
| 2005 Mar 11 | 1435.44 35758 x 35789 x 0.1 GEO 80.1W+0.1E/d | ||
| 2005 Mar 12 | 1436.25 35781 x 35797 x 0.1 GEO 80.1W+0.05W/d | ||
| 2005 Apr 10 | 1436.18 35784 x 35791 x 0.0 GEO 80.1W+0.03/d | ||
Thursday, June 16, 2005
Kosmos 743
1975-053A
There is some question as to whether this vehicle used 11A57 or 11A511U: the NK forum in 2010 said it was actually 11A511U. Unlike most Germes flights, Kosmos-743 made several orbital changes.
| Kosmos-743 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1975 Jun 12 | 1230 | Launch by Soyuz-U | Plesetsk |
| 1234 | Blok-I burn | ||
| 1238 | Blok-I sep | ||
| 1975 Jun 12 | 89.63 179 x 332 x 62.8 | ||
| 1975 Jun 13 | 89.62 180 x 330 x 62.8 | ||
| 1975 Jun 14 | Raise apogee | 89.77 180 x 345 x 62.8 | |
| 1975 Jun 15 | 89.76 180 x 345 x 62.8 | ||
| 1975 Jun 16 | Lower orbit | 89.14 167 x 296 x 62.8 | |
| 1975 Jun 19 | 89.07 167 x 289 x 62.8 | ||
| 1975 Jun 20 | Raise apogee | 89.24 167 x 306 x 62.8 | |
| 1975 Jun 24 | 89.14 166 x 298 x 62.8 | ||
| Engine sep | |||
| 1975 Jun 25 | |||
| 0348? | Deorbit | ||
| 0358? | PO sep | ||
| 0402? | Entry | ||
| 0418? | Landed | ||
Tuesday, June 14, 2005
Gambit-3 32
1971-070A
KH-8 32 was launched on 1971 Aug 12 by Titan IIIB Agena D from Vandenberg on a 22 day flight. This flight was the first to fly the longer focal length R-5 optical system and marked the transition to the long tank Titan 24B. The vehicle was deorbited over Alaska as part of the VAST 3 experiment to recover a 'payload sensor'.
| KH-8 32 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Aug 12 | 1530 | Launch by Titan 3B Agena D | V SLC4W |
| 1532 | Titan stage 1 sep | ||
| 1535 | Titan stage 2 sep | ||
| 1535 | Agena burn | ||
| 1540? | Agena MECO | ||
| 1630 | 90.20 137 x 431 x 111.0 | ||
| 1971 Aug 13 | 0431 | 90.10 136 x 422 x 111.0 | |
| 1971 Aug 15 | 2358 | 89.68 127 x 389 x 111.0 | |
| Orbit raise | |||
| 1971 Aug 16 | 2224 | 90.04 129 x 423 x 111.0 | |
| 1971 Aug 19 | 1623 | 89.87 130 x 405 x 111.0 | |
| Orbit raise | |||
| 1971 Aug 20 | 2220 | 90.05 131 x 422 x 111.0 | |
| 1971 Aug 23 | 1017 | 89.74 131 x 391 x 111.0 | |
| 1946 | SRV-1 deorbit opportunity | ||
| 1953 | Entry | ||
| 2020? | SRV-1 recovered | ||
| Orbit raise | |||
| 1971 Aug 24 | 0847 | 90.06 134 x 420 x 111.0 | |
| 1971 Aug 28 | 2045 | 89.83 132 x 399 x 111.0 | |
| Orbit raise | |||
| 1971 Aug 29 | 2042 | 89.98 134 x 412 x 111.0 | |
| 1971 Sep 1 | 0238 | 89.76 133 x 391 x 111.0 | |
| 1971 Sep 2 | 2023 | 89.48 132 x 365 x 111.0 | |
| 1971 Sep 3 | Reentered after 22d | ||
| 2223? | SRV-2 ejected | ||
| 2230? | Entry | ||
| 2255? | SRV-2 recovered | ||
| 2347? | VAST 3 controlled reentry in Alaska | ||
Friday, June 10, 2005
Kosmos 1298
1981-080A
| Kosmos-1298 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1981 Aug 21 | 1020 | Launch by Soyuz | KB |
| 1028 | Blok-I sep | ||
| 1981 Aug 21 | 89.55 174x331x64.9 | ||
| 1981 Aug 26 | 89.18 166x303x64.9 from 88.96 162x284 | ||
| 1981 Aug 30 | 90.34 164x418x64.9 from 88.71 157x264 | ||
| 1981 Sep 7 | 89.90 151x389x64.9 from 89.26 151x325 | ||
| 1981 Sep 9 | 89.84 177x358x64.9 from 89.56 147x358 | ||
| 1981 Sep 16 | 89.93 194x348x64.9 from 89.21 167x304 | ||
| 1981 Sep 23 | 89.82 188x342x64.0 from 89.13 175x289 | ||
| 1981 Oct 2 | 88.66 166x250x64.9 | ||
| 1981 Oct 2 | 2231? | Landed after 43d | |
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