2013-011A
Second SBIRS HIGH. LMSSC spacecraft with Northrop Grumman Electronic Systems payload .
| SBIRS 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2013 Mar 19 | 2121:00 | Launch by Atlas V 401 AV-037 | CC SLC41 |
| T+4:03 BECO, Az 98.82 | |||
| T+4:09 Atlas sep | |||
| T+4:19 Centaur MES1 11min | |||
| T+4:27 PLF sep | |||
| 2136 | T+15:21 MECO1 174 x 1060? x 26.7? | ||
| 2145 | T+24:07 MES-2 | ||
| 2149 | T+28:02 MECO2 | ||
| 2204 | T+43:19 Centaur sep | 182 x 35804 x 22.19 | |
| 181 x 35934 x 22.2 (webcast) | |||
| 632.6 197 x 35867 x 22.2 (UN) | |||
| 2233? | T+1h12 Blowdown | ||
| 2013 Mar 20? | Apogee burns | ||
2012-040A
Mass 2462 kg; to be located at 10.5 E.
| TL1-03 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2012 Jul 25 | 1543:04 | Launch by CZ-3C Y9 | XSC LC2 |
| T+2:07? Booster sep | |||
| T+2:27? St 1 sep | |||
| T+3:52? Fairing sep | |||
| T+5:32? St 2 sep | |||
| T+5:32? St 3 MES-1 | |||
| 1553? | T+10:31? MECO-1 | 220? x 450? x 28.5? | |
| 1604? | T+21:21? MES-2 | ||
| 1607? | T+24:20? MECO-2 | ||
| 1610? | Stage 3 sep | ||
| 2012 Jul 26 | 765.24 198x 42471 x 18.1 | ||
| 2012 Aug 6 | 1436.11 35771 x 35802 x 2.1 GEO 16.8E | ||
| 2013 May 17 | 1436.13 35782 x 35792 x 1.5 GEO 16.8E | ||
1998-063B
Ariane mission V113 was launched on 1998 Oct 28 from the ELA 2 (Ensemble de Lancement Ariane 2) at the Centre Spatial Guyanais (Kourou, Guyane francaise, South America). V113 was an Ariane 44L model with four strap-on PAL liquid boosters. 18 minutes after launch the LOX/LH2 third stage delivered the two satellite payloads to geostationary transfer orbit.
The upper payload was the first WorldSpace satellite, Afristar. Afristar will broadcast radio, text and video over Africa and the Middle East. Originally planned as a simple L-band satellite for radio broadcasts, the project has grown to include a much larger payload. The satellite is a Matra Marconi Space (Toulouse) Spacebus 2000, using a Marquardt R-4D apogee engine. Prime contractor for the combined satellite and comms payload is Alcatel. Dry mass of Afristar is 1216 kg; it carries 1523 kg of propellant at launch.
The lower payload is the GE-5 satellite, with C and Ku band transponders to augment the GE Americom system. GE Americom contracted with Daimler-Benz Aerospace/Dornier Satellitensystem GmbH/Friedrichshafen to provide the satellite in orbit. They in turn contracted Alcatel/Cannes to provide the Spacebus 2000 satellite, originally built as a backup for Argentina's Nahuelsat. Dry mass of GE 5 is 769 kg; it carries 950 kg of propellant at launch.
GE-5 is a Ku band satellite which will expand the GE Americom system. [898]. The satellite is an Aerospatiale Spacebus 2000. It was built by Alcatel/Cannes for Daimler-Benz Aerospace Dornier Satellitensystem GmbH/Friedrichshafen, which will provide launch and checkout services for GE Americom. The satellite was originally built as a backup Nahuelsat. Launch will be by Ariane 44L V113. Mass is 1719 kg launch, 1013 kg BOL, 769 kg dry.
GE-5 was later called AMC-5 and Americom 5. By 2010 it was in an inclined orbit and no longer suitable for DTH broadcasting; it was replaced by AMC-2 in that role but continued in service for other applications.
| GE-5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1998 Oct 28 | 2215 | Launch by Ariane 44L V113 | CSG ELA2 |
| T+2:30 PAL sep | |||
| T+3:32 St 1 sep | |||
| T+3:35 St 2 burn | |||
| T+4:26 Fairing 01 sep | |||
| T+5:43 St 2 sep | |||
| T+5:48 St 3 burn | |||
| T+18:42 St 2 cutoff | |||
| 2235 | T+20:21 Afristar sep | ||
| 2236 | T+21:31 SMS sep | ||
| 2238 | T+23:30 GE-5 sep | ||
| 2243 | T+28:36 V113 mission complete | ||
| 1998 Oct 29 | 631.15 199 x 35791 x 6.5 | ||
| 1998 Nov 1 | 617.77 195 x 35103 x 6.5 | ||
| 1998 Nov 2? | LAM-1 | ||
| 1998 Nov 4 | 1500? | LAM-2 | |
| 1998 Nov 4 | 1431.31 35525 x 35860 x 0.0 GEO 79.9W+1.1E | ||
| 1998 Dec 16 | 1436.20 35779 x 35798 x 0.0 GEO 79.0W | ||
| 1999 Jan 28 | 1436.13 35772 x 35801 x 0.0 GEO 79.1W | ||
| 1999 Oct 31 | 1436.14 35754 x 35820 x 0.0 GEO 78.9W | ||
| 2006 Aug 3 | 1436.14 35776 x 35798 x 0.0 GEO 79.0W | ||
| 2011 Nov 29 | 1436.18 35764 x 35812 x 1.3 GEO 79.3W | ||
2012-035A
Hughes Network Systems high capacity Ka broadband satellite, built by Loral with over 100 Gbps throughput. Former Spaceway 4, was called Jupiter 1 until it became owned by Echostar, which bought Hughes in 2011.
Hughes Network Systems (Germantown, MD) ordered a Ka-band Loral-1300E satellite with a mass of 6100 kg, for US domestic data comms. Unlike Spaceway 3, no onboard processing will be done.
VA207 performance was 9635 kg (6100 kg Echostar, 2032 kg MSG, 1503 kg adapters and Sylda)
| E17 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2012 Jul 5 | 2136 | Launch by Ariane 5 VA207 | CSG ELA3 |
| T+2:15 EAP sep | |||
| T+3:10 Fairing sep | |||
| T+8:52 EPC burnout | |||
| 2145 | T+8:57 EPC sep | -1064 x 172 x 7.2 | |
| 2145 | T+9:02 ESC-A burn | ||
| 2200 | T+24:51 ESC-A burnout | ||
| 2203 | T+27:28 Echostar sep | ||
| 2207 | T+31:10 Sylda sep | ||
| 2210 | T+34:04 MSG sep | ||
| T+48:55 ESC-A passivation | |||
| 2012 Jul 6 | 632.27 258 x 35789 x 6.0 | ||
| 2012 Jul 7 | 716.79 4528 x 35777 x 3.7 | ||
| 2012 Jul 8 | 872.70 11974 x 35770 x 2.09 | ||
| 2012 Jul 9 | 1013.38 18326 x 35757 x 1.1 | ||
| 2012 Jul 12 | 1426.16 35405 x 35777 x 0.0 GEO 124.8W+2.5E/d | ||
| 2012 Jul 22 | 1436.12 35780 x 35794 x 0.0 GEO 107.1W | ||
| 2013 Jun 6 | 1436.10 35782 x 35790 x 0.0 GEO 107.1W | ||
2009-054A
Astrium/Toulouse Eurostar E3000 for Hispasat services to the Americas. Mass 5465 kg. Size 6.7 x 2.9 x 3.5m, 28m span (Arianespace) or 39m span (EADS) Launch by Ariane 5 in 2009.
| Amazonas 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2009 Oct 1 | 2159 | Launch by Ariane 5ECA L549 | CSG ELA3 |
| 2201 | T+02:13 EAP sep | ||
| T+3:02 Fairing sep | |||
| 2207 | T+8:47 EPC MECO | ||
| T+8:54 EPC sep | -953 x 174 x 6.5 | ||
| 2207 | T+8:58 ESC-A ignition | ||
| 2223 | T+24:34 ESC-A MECO | ||
| 2225 | T+26:59 Amazonas sep | ||
| 2229 | T+30:58 Sylda sep | ||
| 2231 | T+32:54 Comsat sep | ||
| 2009 Oct 1 | 632.34 264 x 35787 x 2.9 | ||
| 2009 Oct 3 | LAM 1 | 782.68 7728 x 35781 x 0.9 | |
| 2009 Oct 4 | LAM 2 | 1087.90 21529 x 35792 x 0.4 | |
| 2009 Oct 5 | 1450? | LAM 3 | 1427.60 35438 x 35802 x 0.1 |
| 2009 Oct 9 | 1428.15 35423 x 35838 x 0.1 GEO 68.1W | ||
| 2009 Oct 13 | 1436.11 35773 x 35800 x 0.1 | ||
| 2009 Nov 19 | 1436.02 35764 x 35806 x 0.1 GEO 67.7W | ||
2012-022A
Launch of the Soyuz TMA-04M spaceship from Baykonur with Gennadiy Padalka , Sergey Revin and Joe Acaba was on May 15.
TMA04M is 11F732A47 No. 705; mission 30S. The SA of vehicle 11F732A47 No. 704 was damaged in ground testing; components of 704 and 705 were combined to make the new vehicle 705.
Mass at docking was 6830 kg.
| TMA4M | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2012 May 15 | 0301 | Launch by Soyuz-FG | |
| T+1:53 SAS sep | |||
| T+1:58 Blok-BVGD sep | |||
| T+2:37 GO sep | |||
| T+4:47 Blok A sep | |||
| T+4:57 KhO sep | |||
| 0309 | T+8:45 Blok-I MECO | ||
| 0309 | T+8:48 Blok-I sep | ||
| 0643:27 | DV1 56s 22.8m/s | ||
| 0735:17 DV2 23s 8.8m/s | |||
| 2012 May 16 | |||
| 0309:20 | DV3 13s 1.0m/s | ||
| 0326s | DV | ||
| 0408s | Braking | ||
| 0418 | In flyaround at 500m | ||
| 0425 | Complete flyaround | ||
| 0426 | Begin final approach | ||
| 0435:56 | Docking with Poisk | ||
| 0716 | HO | ||
| 2012 Sep 16 | |||
| 2012 | HC to ISS | ||
| 2306:00 | Undocking from Poisk, command hooks | ||
| 2308:53 | Undocking | ||
| 2312 | Sep burn | ||
| 2012 Sep 17 | |||
| 0156:18 | DO 4:16 115.2 m/s | ||
| 0200:32 | DO CO | ||
| 0225:29 | Modules sep | ||
| 0228:40 | Entry | ||
| 0238:05s | Chutes deployed | ||
| 0252:53 | Landing | ||
2004-004A
DSP-22 (USA 176) used Titan 4B-39/IUS-10.
| DSP-22 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2004 Feb 14 | 1850 | Launch by Titan 4B-39/IUS-10 | CC SLC40 |
| T+2:12 St 1 burn | |||
| T+2:27 SRMU Sep | |||
| T+3:20 56' fairing sep | |||
| T+5:24 St 1 sep | |||
| 1858 | T+8:58 St 2 MECO | ||
| 1859 | T+9:01 St 2 sep | 93.96 181 x 756 x 28.6 (UN) | |
| 2003:30 | T+1:13:30 SRM-1 | ||
| 2005:55? | SRM-1 burnout | ||
| 2004 Feb 15 | 0119:44 | T+6:29:44 SRM-1 sep | 638.99 375 x 36018 x 28.0 (UN) |
| 0122:56 | T+6:32:56 SRM-2 | ||
| 0144 | T+6:54:51 SRM-2 sep | ||
| 2004 Feb 15? | Aperture cover sep | ||
| 2008 Oct 18 | 1436.12 35741 x 35831 x 1.4 GEO 103.8E | ||
| 2011 Jan 1 | GEO 102E? | ||
| 2011 Dec 15 | 1450.72 36025 x 36118 x 4.2 | ||
| 2012 Feb 18 | 1436.12 35771 x 35803 x 4.3 GEO 70.0E | ||
| 2013 Jan 21 | 1436.12 35776 x 35798 x 5.0 GEO 69.3E | ||
2007-009A
Anik F3 is an EADS Astrium Eurostar E3000 with C, Ku and Ka band capability at 118.7W. Launch mass 4640 kg, span 35.0 m. Launch by ILS Proton/Briz-M.
| Anik F3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Apr 9 | 2254:00 | Launch by Proton 53516 | KB LC200/39 |
| T+2:03 St 1 sep | |||
| T+2:03 St 2 burn | |||
| T+5:30 St 2 MECO | |||
| T+5:31 St 2 sep | |||
| T+5:33 St 3 MES | |||
| T+5:44 GO sep | |||
| 2303:44 | T+9:44 St 3 MECO | ||
| 2303:45 | T+9:45 St 3 sep | -932 x 163 x 51.50 | |
| 2306:19 | T+11:19 Briz MES-1 | ||
| 2312:55 | T+18:55 MECO-1 | 173 x 173 x 51.49 | |
| 2007 Apr 10 | 0002:32 | T+1:08:32 MES-2 | |
| 0019:13 | T+1:25:13 MECO-2 | 258 x 5000 x 50.3 | |
| 0223:44 | T+3:29:44 MES-3 | ||
| 0235:30 | T+3:41:30 MECO-3 | ||
| 0236:09 | T+3:42:09 DTB sep | 316 x 17659 x 49.5 | |
| 0237:39 | T+3:43:39 MES-4 | ||
| 0242:00 | T+3:48:00 MECO-4 | 400 x 35815 x 49.1 | |
| 0746:30 | T+8:52:30 MES-5 | ||
| 0754:22 | T+9:00:22 MECO-5 | 5500 x 35785 x 11.0 | |
| 2007 Apr 10 | 0805:40 | T+9:11:40 Briz sep | 736.73 5514 x 35771 x 11.0 |
| 2007 Apr 14 | LAM | 909.52 13668 x 35767 x 5.0 | |
| 2007 Apr 17 | LAM | 1427.69 35452 x 35790 x 0.1 GEO 125.3W+2.1E/d | |
| 2007 Apr 23 | 1200? | LAM | 1436.09 35781 x 35791 x 0.1 GEO 118.7W |
| 2007 Apr 30 | On orbit delivery to Telesat | ||
| 2013 Jun 17 | 1436.10 35778 x 35794 x 0.0 GEO 118.7W | ||
1997-009A
The first Intelsat 8 satellite was launched by Ariane 4 in Mar 1997. It has 2 C-band spot beams, Ku-band, and a satellite newsgathering (SNG) service. Launch mass was 3420 kg, BOL 2044 kg, dry 1601 kg. The Ariane 44P used fairing 01; Intelsat was the only payload.
| Intelsat 801 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1997 Mar 1 | 0107:42 | Launch by Ariane 44P | CSG ELA2 |
| PAP sep T+1:10 | |||
| Stage 1 sep T+3:32 | |||
| Fairing 01 sep T+4:40 | |||
| Stage 2 sep T+5:43 | |||
| 0126:27 | Stage 3 cutoff T+18:45 | ||
| 0128:22 | H-10-3 sep T+20:43 | ||
| T+21:02 sep burn | |||
| 1997 Mar 1 | 629.88 210 x 35714 x 6.8 | ||
| 1997 Mar 2 | 1430? | LAM-1 | |
| 1997 Mar 2 | 633.81 414 x 35712 x 6.8 | ||
| 1997 Mar 3 | 1200? | LAM-2 | |
| 1997 Mar 3 | 744.38 6262 x 35396 x 3.4 | ||
| 1997 Mar 5 | 0100? | LAM-3 | |
| 1997 Mar 5 | 1142.89 23947 x 35716 x 0.7 | ||
| 1997 Mar 7 | 0800? | LAM-4 | |
| 1997 Mar 9 | 1429.70 35573 x 35749 x 0.0 | ||
| 1997 Mar 10 | 1432.54 35685 x 35748 x 0.0 GEO 46.9E | ||
| 1997 Mar 14 | 1436.03 35773 x 35797 x 0.0 GEO 47.0E | ||
| 1997 Mar 18 | Lost attitude, in spin | ||
| Control recovered | |||
| Testing | GEO 47E | ||
| 1997 Apr 21 | mv out | 1435.92 35764 x 35801 x 0.1 GEO 47.9E | |
| 1997 May 7 s | In service due | GEO 62E | |
| 1997 May 12 | 1436.02 35776 x 35793 x 0.1 GEO 62.0E | ||
| 1997 Dec 10 | 1436.11 35771 x 35803 x 0.1 GEO 62.0E | ||
| 1997 Dec | Move to 64E | ||
| 1997 Dec 18 | 1436.10 35773 x 35796 x 0.1 GEO 64.2E | ||
| 1998 Feb 6 | 1436.15 35775 x 35799 x 0.1 GEO 64.1E | ||
| 1998 Feb 11 | Move out | 1441.00 35859 x 35905 x 0.1 | |
| 1998 Apr 24 | Relocate 31W | ||
| 1998 Apr 29 | 1436.10 35773 x 35799 x 0.1 GEO 31.4W | ||
| 1999 Oct 17 | 1436.11 35762 x 35811 x 0.1 GEO 31.5W | ||
| 2006 Jul 30 | 1436.13 35759 x 35814 x 0.1 GEO 31.5W | ||
| 2010 Mar 1 | 1436.12 35725 x 35849 x 1.4 GEO 31.4W | ||
| 2010 Mar 2 | mv out | ||
| 2010 Mar 9 | mv in | 1436.16 35775 x 35799 x 1.4 GEO 29.5W | |
| 2013 Aug 18 | 1436.12 35771 x 35802 x 4.2 GEO 29.6W | ||
2012-024A
Yantar no. 563. Launch by Soyuz U PVB No. 78031229.
| K2480 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2012 May 17 | 1405:00 | Launch by Soyuz-U | PL LC16 |
| 1409 | Blok-A sep | ||
| 1413:48 | Sep from Blok-I | 88.91 186 x 255 x 81.37 | |
| 2012 Jun 15? | SpK recovery | ||
| 2012 Jul 16? | SpK recovery | ||
| 2012 Sep 24 | Deorbit | ||
| 1639? | Deorbit | -169? x 242 x 81.3 | |
| 1653? | Entry | ||
| 1703? | Landed | ||
