2017-038A
SS/L satellite with 32 Ku-band for fixed sat services and HDTV for Bulgaria Sat AD, a subsidiary set up by Bulsatcom of Stara Zagora.
| BG1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2017 Jun 23 | 1910 | Launch by Falcon 9 | KSC LC39A |
| T+2:36 MECO | |||
| T+2:40 St 1 sep | |||
| T+2:47 SEIG-1 | |||
| T+3:40 Fairing | |||
| 1916 | T+6:19 St 1 entry burn | ||
| 1918 | T+8:20? St1 landing burn | ||
| 1918 | T+8:31 St 1 landing on OCISLY | ||
| 1918 | T+8:38 SECO-1 | ||
| 1937 | T+27:08 SEIG-2 | ||
| 1938 | T+28:13 SECO-2 | ||
| 1944 | T+34:55 BS-1 sep | ||
| 2017 Jul 10 | 212 x 65512 x 24.1 | ||
2017-049A
Formosat-5 prime contractor is NSPO; it will carry a remote sensing instrument from ITRC (Instrument Technology Research Center) of Taiwan.
| F5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2017 Aug 24 | 1851 | Launch by Falcon 9 | V SLC4E |
| T+2:28 MECO 1.877 km/s | |||
| T+2:32 Stage 1 sep | |||
| T+2:53 Fairing | |||
| St 1 apogee 247 km | |||
| 1859 | T+8:45 St 1 entry burn, 3 engines, 39s | ||
| 1900 | T+9:17 Stage 2 SECO | ||
| 1900 | T+9:24 St 1 entry cutoff | ||
| 1901 | T+10:17? St1 landing burn 30s, 1 engine | ||
| 1901 | T+10:47 Stage 1 landing JRTI 31.67N 121.66W | ||
| 1902 | T+11:18 Stage 2 sep | ||
| 2035? | Stage 2 deorbit burn | ||
| 2100? | Stage 2 reentry 166W 42S? | ||
| 2017 Aug 25 | 99.26 717 x 730 x 98.3 | ||
2013-060A
The spacecraft name is Mars Orbiter Satellite; mission name is Mars Orbiter Mission. It was known as Mangalyaan 1 in some media sources but this was not official.
Mars Orbiter Mission is mainly a technology mission, but carries a small, 15 kg, science payload to study the Martian atmosphere and in particular search for methane. However, US scientists claimed that the methane sensor, while able to measure Martian albedo, was not designed properly; background subtraction issues prevented a reliable measurement [839]
ISRO Mars orbiter. HAL structure, ISAC spacecraft. The Insat/IRS derived bus has an improved comms system and a 440N propulsion system designed for restart after a year in cruise. A single solar array is used, made of three 1.4 x 1.8m panels, with the 2.2m dia HGA on the opposite side. Box + panel + dish. 1337 kg probe full (850 kg prop, 500 kg dry) in 370 x 80000 km orbit. Mass prior to MOI was 801.3 kg. Mission requires 2.592 km/s. Comms via Indian Deep Space Station IDSN32, a 32-m antenna in Bangalore/Byalalu.
The PSLV-XL has 6 PSOM-XL, the S139 core, PL40 stage 2, HPS3 stage 3, L2.5 stage 4.
| MOM | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2013 Nov 5 | 0908 | Launch by PSLV-XL C25 | SDSC |
| T+0:25 PSOM 5-6 on | |||
| T+1:10 PSOM 1-2 sep | |||
| T+1:10 PSOM 3-4 sep | |||
| T+1:32 PSOM 5-6 sep | |||
| T+1:52 PS1 sep | |||
| T+1:53 PS2 burn | 58 km, 2.387 km/s | ||
| T+3:21 Fairing | 113 km, 3.625 km/s | ||
| 0912 | T+4:24 PS2 sep | ||
| 0912 | T+4:26 PS3 burn 132 km, 5.379 km/s | -4364 x 132 | |
| 0917 | T+9:43 PS3 sep | -70? x 300? | |
| Long coast, 27:24 | |||
| 0943 | T+35:00 PS4 burn 271 km, 7.642 km/s | -70? x 300? | |
| 0951 | T+43:39 PS4 off | 342 km, 9.833 km/s | |
| 0952 | T+44:16 Stage 4 sep | 251 x 23892 x 19.35 | |
| 247 x 23563 x 19.27 (ISRO) | |||
| 2013 Nov 6 | 1947 | Peri burn 1 | 250 x 28814 km |
| 2013 Nov 7 | 2048:51 | Peri burn 2 570.6s | x 40186 km |
| 2013 Nov 8 | 1940:43 | Peri burn 3 707s | x 71636 km |
| 2013 Nov 10 | Peri burn 4 35m/s | x 78276 | |
| 2013 Nov 11 | 2333:50 | Peri burn 4b 303.8s | 276 x 118642 x 19.3 |
| 2013 Nov 15 | 1957 | Peri burn 5 243s 101.6m/s | x 192874 |
| 853 x 194683 x 19.4 | |||
| 2013 Nov 16 | 1503 | Pass EL1:4 | |
| 2013 Nov 30 | 1919 | Peri burn 6, SOI to Mars Transfer Traj 648m/s 1351s 198 kg | |
| 1328.9s 647.96 m/s | |||
| 2013 Dec 5 | 2056 | Leave Earth Hill sphere 1.5Mkm | |
| 2013 Dec 11 | 0100 | TCM-1 40.5s burn; R=2.9Mkm | |
| 2014 Jun 11 | 1100 | TCM-2 16s 1.577m/s | |
| 2014 Aug | TCM-3 cancelled | ||
| 2014 Sep 20 | 0427 | Mars sphere 1.08Mkm | |
| 2014 Sep 22 | 0040 | Mars SOI | |
| 2014 Sep 22 | 0900s | TCM-4 4.0s 0.6kg 2.1m/s | |
| 2014 Sep 24 | 0200 | MOI 1.099km/s | 3.66d 365 x 80000 x150.0 |
| 0142 | Eclipse starts | ||
| 0147:32 | MOI burn (SCET) 515 km 24:14 249.5 kg 1098.7m/s | ||
| 0207 | Eclipse ends | ||
| 0211:46 | MOI CO, 40 kg prop left | ||
| 4371.85 419 x 76872 x 150.04 | |||
| 0217 | Resume telem | ||
| 2014 Oct 5 | 392 x 76776 x 150.1 | ||
| 2014 Oct 6 | 0445 | TCM to avoid comet, 1.9 km | 392 x 70998 x 150.1 |
| 2015 Mar 24 | Primary mission complete, 37 kg prop remain | ||
| 2015 Jun 6 | Begin conjunction | ||
| 2015 Jun 22 | End conjunction | ||
| 2017 Jan 17 | 500 x 71050 x 150 | ||
2007-035A
EMU spacesuits for four STS-118 spacewalks: 3010 (Mastracchio), 3017 (D.Williams), 3008 (Anderson)...
3010 and 3017 transfer to ISS and then back.
Cargo transfer 6686 kg total dry plus 467 consumables, 1495 return; per SODB 5366 kg transfer, 5325 kg PLB not deployed, 143 kg return (including about 100 kg MISSE).
Per mission report, 367 kg MD to ISS, 1353 kg SHAB to ISS, 4965 kg S5+ESP3. ISS to MD 184 kg (including MISSE), ISS to SHAB 1311 kg, STS to ISS 467 kg consumables (of which 46 kg to Quest HPGAs).
If S5 is 1815 kg, then ESP3 is 3150 kg.
| STS-118 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2007 Jul 2 | In OPF/2 | ||
| 2007 Jul 2 | Rollover to VAB | ||
| 2007 Aug 8 | 2236:42 | Launch | KSC LC39A |
| 2238:45 | SRB sep | ||
| 2245:07 | MECO | ||
| 2245:29 | ET sep | ||
| 2313:42 | OMS-2 2:45 | ||
| 2316:27 | OMS-2 CO | ||
| 2346? | ET reentry | ||
| 2007 Aug 9 | 0011:46 | PLBD open | 229 x 317 x 51.6 |
| 0136:15 | OMS-3 NC1 | 226 x 319 x 51.6 | |
| 0137:07 | OMS 3 CO | ||
| 301 x 329 x 51.6 | |||
| 1436:18 | OMS-4 NC2 15s burn 112855 kg OMS both | ||
| 1436:33 | OMS 4 CO | ||
| 2007 Aug 10 | 0222s | NC3 | |
| 1345:44 | OMS-5 NC4 11.8fps 112368 kg | ||
| 1345:59 | OMS 5 CO | ||
| 1515? | TI burn RCS 9s | 91.36 335 x 346 x 51.6 | |
| 1650 | On R-bar at 240m | ||
| 1656 | Begin RV pitch mvr | ||
| 1705 | Complete RPM | ||
| 1710 | Begin flyaround on nadir R-bar | ||
| 1724 | At +Vbar 112m | ||
| 1731 | At 100m, approach along Vbar | ||
| 1749 | 30m range to ISS | ||
| 1757 | 10m, final approach | ||
| 1801:56 | Docked to PMA-2 | ||
| 1950 | RMS in motion to grapple S5 | ||
| 1959 | RMS grapple S5 | ||
| 2004 | HO to ISS | ||
| 2043 | S5 PRLA release | ||
| 2050 | RMS unberth S5 | ||
| 2117 | SSPTS activated for first time | ||
| 2128? | SSRMS grapple S5 | ||
| 2130? | RMS ungrapple S5 | ||
| Mass: 109954 kg | |||
| 2007 Aug 11 | EVA-1 | ||
| 1608 | At 5 psi, holding | ||
| 1611 | Resume depress | ||
| 1614 | At 2 psi? | ||
| 1624? | Depress | ||
| 1625 | At 0.5 psi | ||
| 1626 | 23mm | ||
| 1628 | HO | ||
| 1629 | Battery power | ||
| 1637 | Mastracchio egress | ||
| 1641 | Williams egress | ||
| 1705 | S5 3m from S4 | ||
| 1730 | S5 soft capture on 2 corners | ||
| 1735 | S5 soft capture complete, bolts torquing | ||
| 1753 | S5 bolts torqued | ||
| 1755 | S5 go for ungrapple | ||
| 1827 | S5 hard mated | ||
| 1847 | Grapple fixture relocation | ||
| 1940 | Fixture relocated to keel | ||
| 2045 | Cleaning up S5 work | ||
| 2055 | In airlock recharging | ||
| 2128 | Retract P6 radiator No 3 | ||
| 2134 | Retract complete | ||
| 2230? | Ingress EV2 | ||
| 2234 | Ingress EV1? | ||
| 2241 | HC | ||
| 2245 | Repress | ||
| 2007 Aug 12 | 0050 | MT moving to WS4 | |
| 0135 | MT due to move to WS7 | ||
| SSRMS grapple OBSS | |||
| SSRMS hand OBSS to SRMS | |||
| 1913 | Focussed inspection complete | ||
| 1919 | SSRMS grapple OBSS (from SRMS) | ||
| 1936 | SRMS ungrapple OBSS | ||
| 1955 | OBSS berthed | ||
| 2027 | SSRMS grapple Lab | ||
| 2007 Aug 13 | EVA-2 Mastracchio, Williams | ||
| 1526? | Depress | ||
| 1528 | TC open | ||
| 1529 | HO | ||
| 1532 | On BP | ||
| 1536 | Egress EV2 Williams | ||
| 1539 | Egress EV1 Mastrac. | ||
| 1550 | Working at CMG-3 on Z1 | ||
| 1626 | CMG-3 removed from Z1 | ||
| 1631 | CMG-3 on Z1 handrail ball stack bracket | ||
| 1735? | New CMG-3R ORU unberthed | ||
| 1822 | CMG ORU on ESP-2 | ||
| 1851 | CMG unberthed from ORU frame | ||
| 1926 | CMG-3R installed in Z1 | ||
| 2020? | CMG-3 installed in frame on ESP-2 | ||
| 2114? | CMG-3 work complete | ||
| 2150? | Ingress | ||
| 2151 | TC | ||
| 2157 | HC | ||
| 2200 | Repress | ||
| 2007 Aug 14 | |||
| 1313 | ESP-3 grappled by SRMS | ||
| 1340? | ESP-3 unberthed | ||
| 1450? | ESP-3 grappled by SSRMS from SRMS | ||
| 1618? | ESP-3 attached to P3 | ||
| 2007 Aug 15 | EVA-3 Mastracchio, Anderson | 91.35 335 x 346 x 51.6 | |
| 1434 | Depress | ||
| 1436 | HO | ||
| 1437 | BP | ||
| 1455? | Egress EV1 | ||
| 1459? | Egress EV2 | ||
| 1530 | M. relocating SASA from P6 to P1 | ||
| 1705 | Anderson moving CETA 1 from P1 | ||
| 1728 | CETA 1 locked on S1 | ||
| 1745 | Anderson moving CETA 2 from P1 | ||
| 1802 | CETA 2 locked on S1 | ||
| 1850 | Glove damage seen on Mastracchio | ||
| 1855 | Ingress Mastracchio early for glove damage | ||
| 1951 | Ingress Anderson | ||
| 1952 | TC closing | ||
| 1955 | TC closed | ||
| 2000 | HC | ||
| 2005 | Repress | ||
| 2007 Aug 18 | EVA4, Williams, Anderson | ||
| 1314 | Depress | ||
| 1316 | HO | ||
| 1317 | BP | ||
| 1325 | Egress Williams | ||
| 1335 | Egress Anderson | ||
| 1420 | Install OBSS clamps on S1 truss | ||
| 1500 | Retrieve 2 MISSE packs (MISSE-3, 4) | ||
| 1630? | EWIS antenna installed on Destiny | ||
| 1802 | Ingress Anderson | ||
| 1803 | Ingress Williams | ||
| 1805 | TC closed | ||
| 1814 | HC | ||
| 1819 | Repress (NASA: 5:02) | ||
| 2000? | Transfer 3010/3017 to STS | ||
| 2110 | ISS side HC | ||
| 2007 Aug 19 | 1156:27 | Undocking along V-bar | |
| 1226? | 120m on V-bar, sep-1 burn | ||
| 1248 | On zenith R-bar, sep-2 burn 4s 0.5m/s | ||
| 2007 Aug 21 | 1252:28 | PLBD closed | 91.38 336 x 347 x 51.6 |
| 1525:12 | OMS DO 3:35 110.0m/s | ||
| 1528:47 | OMS DO CO | -28 x 342 x 51.6 | |
| 1600:27 | EI | ||
| 1632:17 | MGTD KSC RW15 | ||
| Landing mass 100878 kg | |||
| 1632:29 | NGTD | ||
| 1633:20 | Wheels stop | ||
| 2210 | Tow to OPF/2 | ||
2004-031A
Hispasat Amazonas 1 will be at 61W, operated by the Brazilian Hispamar subsidiary, with control center in Rio de Janeiro. 4540 kg, 35-m span Astrium Eurostar 3000 satellite.
Launch with Proton-M 53507 Briz-M 88510 in Aug 2004. A problem in the oxidizer tank pressurization reduced propulsion ability and caused an insurance claim.
In 2014 Hispasat relocated the satellite to an Intelsat slot at 55.5W, and joined forces with Intelsat to use it and other colocated satellites (Galaxy 11 and IS-805) for World Cup coverage.
| Amazonas | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2004 Aug 4 | 2232:00 | Launch by Proton-M/Briz-M | KB LC200/39 |
| T+2:03 St 1 sep | |||
| T+5:33 St 2 sep | -4900? x 140? x 51.6 | ||
| T+5:46 Fairing sep 125 km 4.5 km/s | -4900? x 140? x 51.6 | ||
| T+9:34 Stage 3 MECO | |||
| 2241 | T+9:47 Stage 3 sep 7.20 km/s 150 km | -900? x 170? x 51.6 | |
| 2243 | T+11:20 Briz MES-1 | ||
| 2250 | T+18:49 Briz MECO-1 | 173 x 173 x 51.5 | |
| 2340 | T+1:08:08 Briz MES-2 | ||
| 2356 | T+1:24:41 Briz MECO-2 | 258 x 5000 x 50.3 | |
| 2004 Aug 5 | |||
| 0200 | T+3:28:55 Briz MES-3 | ||
| 0212 | T+3:40:13 MECO-3 | ||
| 0213 | T+3:41:06 DTB sep | 297.45 315 x 16648 x 49.5 | |
| 0214 | T+3:42:08 MES-4 | ||
| 0218 | T+3:46:57 MECO-4 | 395 x 35820 x 49.1 | |
| 0724 | T+8:52:21 MES-5 | ||
| 0731 | T+8:59:55 MECO-5 | 3200 x 35786 x 9.1 | |
| 0743 | T+9:11:20 Briz sep | ||
| 2004 Aug 5 | 1310 | 689.13 3142 x 35789 x 9.1 | |
| 2004 Aug 7 | 0319 | 836.32 10286 x 35765 x 4.6 | |
| 2004 Aug 7 | 1435 | 1198.00 26170 x 35802 x 1.1 | |
| 2004 Aug 14 | 1226.40 26145 x 37004 x 1.2 | ||
| 2004 Aug 15 | LAM? | ||
| 2004 Aug 19 | 1436.05 35782 x 35788 x 0.1 GEO 61.0W | ||
| 2004 Aug 27 | 1436.08 35781 x 35791 x 0.1 GEO 60.9W | ||
| 2004 Oct 13 | 1436.07 35769 x 35802 x 0.1 GEO 60.9W | ||
| 2006 Aug 8 | 1436.11 35777 x 35796 x 0.0 GEO 61.0W | ||
| 2013 Apr 14 | 1436.09 35768 x 35804 x 0.1 GEO 61.0W | ||
| 2013 Apr | Replaced by Amazonas 3 | ||
| 2013 Apr | Plan to move to 36W | ||
| 2013 May 22 | 1436.17 35758 x 35817 x 0.1 GEO 61.1W | ||
| 2013 May 26 | Move out of 61W | ||
| 2013 May 31 | Stop at 48W | ||
| 2013 Jul 9 | 1436.07 35773 x 35798 x 0.1 GEO 48.0W | ||
| 2013 Sep 2 | 1436.06 35774 x 35796 x 0.0 GEO 48.0W | ||
| 2013 Sep 7 | Leave 48W | ||
| 2013 Sep 22 | Arrive 36W | 1436.13 35777 x 35797 x 0.1 GEO 36.1W | |
| 2014 Feb 13 | 1436.11 35779 x 35794 x 0.0 GEO 36.0W | ||
| 2014 Feb 21 | Move out | ||
| 2014 Mar 19 | Arrive 55W Intelsat location | ||
| 2014 May 23 | 1436.14 35777 x 35797 x 0.1 GEO 55.4W | ||
| 2016 Jun 5 | Move out | 1436.17 35771 x 35804 x 1.0 GEO 55.4W | |
| 2016 Jul 11 | move in | 1436.05 35773 x 35798 x 1.0 GEO 36.2W | |
| 2017 Jun 19 | 1436.17 35770 x 35805 x 1.8 GEO 36.4W | ||
