Saturday, July 3, 2010
Kosmos 2336
1996-071A
Kosmos-2336 was launched in Dec 1996.
| Kosmos-2336 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1996 Dec 20 | 0643:58 | Launch by Kosmos-3M | PL LC132 |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| 0646 | T+2:12 St 2 burn 59km | ||
| 0646 | T+2:27 Fairing 76km | ||
| 0652 | T+8:03 St 2 MECO 150 km | 150 x 1003? x 83 | |
| 0746 | T+1:02:19 St 2 MES2 | ||
| 0746 | T+1:02:30 St 2 MECO2 | ||
| 0747 | T+1:03 St 2 sep | ||
| 1996 Dec 20 | 105.03 979 x 1012 x 83.0 | ||
| 2008 Sep 2 | 105.00 976 x 1012 x 82.9 | ||
Measat 3A
2009-032A
Orbital Star at 91.5E, colocated with Measat 3. 2366 kg (Sea-Launch MO) or 2417 kg (AWST 081117-16).
12 Ku, 12 C, 3 antennas.
Fixed satellite C-band services in Asia and Mideast; Ku TV broadcasting to Malaysia and Indonesia.
Launch 2008 by Zenit-3SLB with Zenit-2SB60 No. 3 core stage and DM-SLB No. 3L upper stage. Originally to be called Measat 1R, but renamed before launch. Stage 2 impact range is 6850 km.
| Measat 3A | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2009 Jun 21 | 2150 | Launch by Zenit-3SLB | KB |
| T+2:29 Stage 1 sep 83 km | |||
| T+5:17 Fairing sep 204 km | |||
| 2158 | T+8:31 Stage 2 sep | -2094 x 297 x 51.34 | |
| T+8:41 DM MES-1 | -2094 x 302 x 51.34 | ||
| 2202 | T+11:59 MECO-1, 363 km | 190 x 533 x 51.35 | |
| 2309 | T+1:19:09 DM MES-2 201 km | 196 x 555 x 51.35 | |
| 2314 | T+1:24:35 MECO-2, 338 km | 202 x 35854 x 49.0 | |
| 2009 Jun 22 | 0402 | T+6:12:05 DM MES-3 | |
| 0403 | T+6:13:59 MECO-3 | 11620 x 35586 x 10.63 | |
| 0414 | T+6:24:49 DM sep, over Sumatra | ||
| 2009 Jun 22 | 860.95 11587 x 35609 x 10.6 | ||
| 2009 Jun 23 | 990.61 17438 x 35640 x 6.1 | ||
| 2009 Jun 27 | 1248.56 28285 x 35776 x 2.28 | ||
| 0450? | LAM | ||
| 2009 Jun 27 | 1433.31 35683 x 35780 x 0.0 GEO 90.5E+0.7E/d | ||
| 2009 Jul 1 | 1436.13 35782 x 35792 x 0.04 GEO 91.5E | ||
| 2010 Apr 29 | 1436.22 35778 x 35799 x 0.0 GEO 91.5E | ||
Friday, July 2, 2010
HTV-2a
2010-S30
Minotaur IV Lite launch, USAF/DARPA V to KMR BOA, 75-150 km north of KMR Roi-Namur, say 167.5E 10.5N 4m long, 900 kg. DARPA, LM/Valley Forge? HTV-2 Mission A. Apogee around 45-60 km?. 30 min flight. Mach 15-20; at this alt Mach 1 = 315-330 m/s so Mach 15-20 = 4.7 to 6.3 or 5.0 to 6.6 km/s pro
| HTV2a | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2010 Apr 22 | 2300 | Launch by Minotaur IV Lite | V SLC8 |
| T+0:56 Stage 1 sep | |||
| T+1:55 Stage 2 sep | |||
| T+2:05 Fairing sep | |||
| 2303 | T+3:00 Stage 3 burnout 60 km? | ||
| T+3:00? Stage 3 sep | |||
| HTV apogee | 100? | ||
| HTV maneuvering | |||
| T+30:00? Ocean impact | |||
Thursday, July 1, 2010
Ofeq 9
2010-031A
'Ofeq-9 was launched in 2010 (TECSAT was renamed 'Ofeq-8.)
| Ofeq 9 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2010 Jun 22 | 1900? | Launch by Shavit | PAL |
| Stage 1 MECO at T+0:52 | |||
| 1901? | Stage 1 sep | ||
| Stage 2 MECO at T+1:44, | |||
| 1902? | Stage 2 sep, 110 km | ||
| 1907? | Fairing (2 pieces) sep, 250 km | ||
| 1907? | Main equipment compartment sep | ||
| 1909? | Stage 3 92s burn over W Med. | ||
| 1910? | Stage 3 sep | 294 x 595 x 141.8 | |
Monday, June 28, 2010
Intelsat 14
2009-064A
IS-14 is a Loral 1300 satellite to replace PAS-1R (IS-1R). As an auxiliary payload, it carries DoD's IRIS project to demonstrate direct routing of miliary comms over IP.
Mass 5663 kg full, 2517 kg dry.
Located at 45W. Launch by Atlas V 431 with 4-m XEPF fairing.
| IS-14 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2009 Nov 23 | 0655:00 | Launch by Atlas V 431 AV-024 | |
| T+2:08 SRB sep | |||
| T+4:33 Stage 1 sep | |||
| T+4:43 MES-1 | |||
| 0659 | T+4:51 Fairing sep | ||
| 0713 | T+18:24 MECO-1 | 175 x 25998 x 25.0 | |
| 0848 | T+1:53:24 MES-2 1:33 | ||
| 0849 | T+1:54:56 MECO-2 | ||
| 0853 | T+1:58:02 Centaur sep | ||
| 2009 Nov 24 | 819.32 6157 x 39094 x 22.45 | ||
| 2009 Nov 25 | 886.08 9269 x 39092 x 6.9 | ||
| 2009 Nov 27 | 1093.88 18484 x 39094 x 15.9 | ||
| 2008 Nov 29? | LAM | ||
| 2009 Nov 30 | 1444.10 35092 x 36794 x 0.05 | ||
| 2009 Dec 8 | 1436.11 35772 x 35800 x 0.0 GEO 46.9W | ||
| 2010 Jan 22 | 1436.06 35776 x 35796 x 0.0 GEO 45.0W | ||
Molniya 352
2001-050A
According to NPO PM Newsletter No 126, this satellite was Molniya-3 No. 64.
| Molniya-3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2001 Oct 25 | 1134:13 | Launch by 8K78M | PL LC43/3 |
| 1136:08 | BVGD sep | ||
| 1136:58 | GO sep | ||
| 1138:59 | T+4:46 Blok A sep | ||
| 1139:09 | T+4:56 KhO sep | ||
| 1142:59 | T+8:46 Blok-I MECO | ||
| 1143:03 | T+8:50 Blok-I sep | 214 x 617 x 62.8 | |
| 1227:29 | T+53:16 BOZ burn | ||
| 1228:09 | T+53:56 BOZ sep | ||
| 1228:09 | ML burn | ||
| 1230:59 | T+56:46 ML MECO | ||
| 1231:07 | T+56:54 ML sep | 615 x 40659 x 62.8 | |
| 1231 | Mol-3 and ML perigee at 620 km over 56S 113W | ||
| 1234 | Blok I apogee at 617 km over 53S 108W | ||
| 2004 Nov 5 | Orbit correction | 717.69 491 x 39859 x 64.7 | |
| 2006 Aug 4 | 717.79 1218 x 39137 x 64.9 | ||