Thursday, March 20, 1997
Saturn S-IVB-509
1971-008B
SA-509 was launched on 1971 Jan 31 at 2103. The S-IVB-509 stage impacted the lunar surface at 0740:54 on Feb 4.
| S-IVB-509 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Jan 31 | 2103:02 | Launch by Saturn V (SA-509) | KSC LC39A |
| 2105:17 | S-IC CECO | ||
| 2105:45 | S-IC OECO | ||
| 2105:47 | S-IC sep, S-II ignition | ||
| 2106:16 | Interstage sep | ||
| 2106:22 | LES jet | ||
| 2107:33 | T+4:31 S-IC apogee 116.5 km | ||
| 2110:45 | S-II CECO | ||
| 2112:08 | S-IC impact 74.052W 29.835N | ||
| 2112:21 | S-II OECO, sep | ||
| 2112:22 | S-IVB ignition | ||
| 2112:33 | Ullage case jettison | ||
| 2113:02 | S-II apogee 190 km | ||
| 2114:42 | S-IVB cutoff | ||
| 2114:51 | Earth orbit insertion | 183 x 189 x 31.11 | |
| 185 x 185 x 31.11 (MPR) | |||
| 2123:48 | T+20:46 S-II imapct 29.05N 33.57W | ||
| 2331:33 | S-IVB TLI burn | ||
| 2337:24 | S-IVB cutoff | ||
| 2337:34 | Translunar injection at 337 km | 221 x 460000 x 30.81 | |
| 1971 Feb 1 | 0005:32 | CSM sep from SLA/S-IVB | |
| 1971 Feb 1 | 0307:03 | T8+1s APS evasive, 80s, 2.9m/s | |
| 0323:42 | T8+1000s CVS vent 300s, 2.3m/s | ||
| 0328:22 | T8+1280s LOX vent, 48s, 8.8m/s | ||
| 0603:00 | T8+10558s APS impact burn 252s 10.3m/s | 106 x 420757 | |
| 0607:12 | APS burn complete | ||
| 1971 Feb 1 | 1425 | Pass EL1:4 | |
| 1971 Feb 2 | 0005? | Pass 200000 km | |
| 1971 Feb 3 | 1502 | Lunar SOI | |
| 1971 Feb 4 | 0740:54 | Impact | -1468 x Inf |
Kosmos 2054
1989-101A
The third Al'tair satellite was launched in Dec 1989 and began operations in early 1990.
| Kosmos-2054 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Dec 27 | 1110:00 | Launch by Proton | KB |
| 1119 | Stage 3 sep | 182 x 190 x 51.6 | |
| 1226? | DM burn 1 | 363 x 36361 x 47.3 | |
| 1749? | DM burn 2 | ||
| 1753? | DM sep | ||
| 1990 Jan 1 | 1469.58 36375x36503x1.5 | ||
| 1990 Jan 10 | 1449.28 35964x36123x1.5 7.0W+3.9W | ||
| 1990 Feb 5 | 1436.84 35744x35859x1.4 GEO 16.4W+0.2W | ||
| 1990 Feb 26 | 1435.98 35766x35802x1.3 GEO 15.9W+0.02 | ||
| 1990 Feb 28 | 1435.98 35767 x 35800 x 1.3 GEO 15.8W | ||
| 1990 Apr 7 | 1436.12 35764 x 35809 x 1.3 GEO 15.7W | ||
| 1991 Jan 19 | 1436.11 35780 x 35793 x 0.6 GEO 16.1W | ||
| 1991 Dec 28 | 1436.15 35781 x 35793 x 0.3 GEO 15.9W | ||
| 1992 Sep 25 | 1436.10 35767 x 35805 x 1.0 GEO 16.0W | ||
| 1993 Jun 30 | 1436.09 35763 x 35809 x 1.6 GEO 15.7W | ||
| 1994 Mar 21 | 1436.09 35773 x 35799 x 2.1 GEO 16.4W | ||
| 1995 Jun 17 | 1436.14 35765 x 35809 x 3.1 GEO 15.6W | ||
Tuesday, March 18, 1997
Leasat 3
1985-028C
When Leasat 3 (Syncom IV F3) was deployed from Discovery on mission 51-D in Apr 1985, it failed to activate itself. A power switch on the side of the satellite was meant to be tripped as the satellite left the cargo bay and turn on the systems, but the satellite remained inert. Discovery completed a re-rendezvous with the satellite and attempted to trip the switch with a makeshift `flyswatter' attached to the end of the remote manipulator arm, but to no avail - an internal short circuit was to blame. With the satellite inert and trapped in a decaying low Earth orbit, a rescue mission was mounted. Shuttle flight 51-I flew to the satellite in August, and astronaut James Van Hoften grabbed it out of orbit. After repairs, he released it again and the satellite began to operate normally. Several months later, the perigee motor was successfully fired.
| Syncom IV F3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 Apr 13 | 1458:22 | Deploy from OV103 | |
| Failed to activate | |||
| 92.30 314 x 460 x 28.5 | |||
| 1985 Apr 17 | 1400 | Rendezvous Syncom | |
| 1412 | RMS contact with Leasat 3 | ||
| RMS tripped power switch, | |||
| still inactive | |||
| 1418 | Last RMS contact with Leasat 3 | ||
| 1801 | 92.31 315 x 459 x 28.5 | ||
| 1985 Apr 27 | 92.29 315 x 458 x 28.5 | ||
| 1985 Jul 6 | 92.22 314 x 452 x 28.5 | ||
| 1985 Aug 28 | 92.18 313 x 449 x 28.5 | ||
| 1985 Aug 31 | 1220 | Leasat 3 rendezvous | |
| 1400 | MS2 captures Leasat | ||
| 1518 | RMS grapple Leasat | ||
| Leasat repairs | |||
| 1985 Sep 1 | 92.17 313 x 448 x 28.5 | ||
| 1985 Sep 1 | 1230? | Leasat repairs | |
| 1509 | MS2 deploy Leasat | ||
| 1985 Oct 15 | 92.14 312 x 447 x 28.5 | ||
| 1985 Oct 25 | 92.09 308 x 445 x 28.5 | ||
| 1985 Oct 27 | 1153 | Reported PKM burn time? (or EST) | |
| 1655 | PKM burn based on TLE, over 150E 0N | ||
| 1656 | PKM cutoff | 288.68 316 x 15864 x 27.0 | |
| 2348? | PKM jettison | ||
| 1985 Oct 28 | 0232 | LAM Perigee burn 1 | 356.35 314 x 20228 x 26.9 |
| 1985 Oct 28 | 2020? | LAM peri burn 2 | 480.54 314 x 27575 x 27.0 |
| 1985 Oct 29 | 2020? | LAM peri burn | 639.74 289 x 36142 x 26.9 |
| 1985 Oct 30 | 0100? | LAM apo burn | 729.41 4800 x 36047 x 15.3 |
| 1985 Oct 31 | 0200? | LAM apo burn | 1438.60 35604 x 36067 x 15.3 |
| 1985 Nov 11 | 1435.90 35596 x 35968 x 3.2 GEO 174.9W | ||
| 1985 Nov | Leasat PAC | GEO 175W | |
| 1986 Nov 30 | 1435.92 35781 x 35784 x 2.3 GEO 176.8W | ||
| 1986 Dec 10 | mv out | 1435.87 35780 x 35784 x 2.3 GEO 176.3W+0.05E | |
| 1986 Dec 30 | 1426.52 35416 x 35777 x 2.2 GEO 130.2W+2.4E | ||
| 1987 Feb 12 | mv in Leasat CONUS | 35781 x 35789 x 2.1 GEO 104.9W | |
| 1988 Dec 23 | 1436.09 35772 x 35800 x 0.8 GEO 105.6W | ||
| 1990 Feb 6 | 1436.12 35767 x 35806 x 1.0 GEO 104.7W | ||
| 1993 Sep 20 | 1436.08 35774 x 35798 x 3.9 GEO 105.9W | ||
| 1995 Mar 12 | 1436.11 35765 x 35808 x 4.9 GEO 104.9W | ||
| 1996 Sep 30 | 1436.07 35774 x 35797 x 5.9 GEO 104.9W | ||
Progress M-8
1991-038A
Progress M 11F615A55 No. 207 (Progress M-8) carried 2693 kg of cargo including a cosmic ray experiment from UC Berkeley and a replacement rendezvous antenna for the Kvant module, as well as a 10m diameter balloon subsatellite to measure upper atmospheric air density.
| Progress M-8 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1991 May 30 | 0804:03 | Launch by Soyuz-U | KB |
| 0850 | 88.65 186 x 230 x 51.6 | ||
| 1430 | 90.22 281 x 290 x 51.6 | ||
| 1991 May 31 | 1200 | 90.23 281 x 290 x 51.6 | |
| 1991 Jun 1 | 0944:37 | Docked at Mir DP1 | |
| 1200 | 91.88 363 x 370 x 51.6 | ||
| 1991 Jun 3 | 2052 | 91.86 361 x 370 x 51.6 | |
| 1991 Jun 7 | Orbit correction | ||
| 1991 Aug 15 | 2216:59 | Undocked | |
| Stationkeeping | |||
| 1991 Aug 16 | 1035 | Eject balloon cover | |
| 1038 | Eject balloon subsatellite 86-17FJ | ||
| 1412 | Balloon burst | ||
| 1991 Aug 17 | 0600 | Deorbited over Pacific | |
| 0656:32 | Reentered | ||
Kosmos 839
1976-067A
Kosmos 839 was intercepted by Kosmos 843.
| Kosmos-839 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1976 Jul 8 | 2108 | Launch by 11K65M | PL |
| 2116? | Stage 2 MECO-1 | ||
| 2134? | Stage 2 MECO-2 | ||
| 2134? | Stage 2 sep | ||
| 1976 Jul 8 | 116.9 984x2098x65.9 | ||
Resurs 46
1990-082A
Resurs F-1 14F43 No. 51, the 9th acknowledged Resurs F, was launched in Sep 1990. The vehicle carried a German Intospace company experiment called Casimir, designed to make zeolite crystals.
| Resurs F-1 14F43 No. 51 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Sep 7 | 1200 | Launch by Soyuz-U | PL LC16 |
| 1208 | Blok-I sep | 88.72 180 x 241 x 82.5 | |
| 1990 Sep 8 | 88.91 180 x 260 x 82.5 | ||
| 0500 | 89.86 261 x 274 x 82.57 | ||
| 1990 Sep 15 | 89.81 258 x 271 x 82.57 | ||
| 1200 | 89.86 260 x 274 x 82.57 | ||
| 1990 Sep 20 | 89.81 258 x 271 x 82.57 | ||
| 1990 Sep 22 | |||
| 0706? | Deorbit | ||
| 0714? | PO sep | ||
| 0723? | Entry | ||
| 0738? | Landed | ||
Monday, March 17, 1997
Soyuz TM-14
1992-014A
The Russian-German crew of Viktorenko, Kaleri and Flade were launched in Mar 1992 aboard 11F732 No. 64, Soyuz TM-14. The same crew returned to Earth in Aug 1992.
| Soyuz TM-14, Flight 1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1992 Mar 17 | 1054:30 | Launch by Soyuz-U2 | KB LC1 |
| 1103 | Blok-I cutoff | ||
| 1992 Mar 19 | 1025:43 | TCM | |
| 1120:20 | TCM | ||
| 1150 | TCM | ||
| 1232:50 | Docked 37KE +X | ||
| 1400? | Hatch open | ||
| Soyuz TM-14, Flight 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1992 Aug 9 | 1830 | Hatch closed | |
| 2146:47 | Undocked 37KE +X | ||
| 1992 Aug 10 | 0008 | Deorbit 261s | |
| 0012 | DO CO | ||
| 0036? | Modules sep | ||
| 0042? | Entry | ||
| 0105:02 | Landed | ||
May 13,2026
https://planet4589.org/space/jsr/back/news.855.txt
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