1974-101A
The Symphone MV1 (flight model 1) satellite was launched on 1974 Dec 19 from Cape Canaveral. Launch was successful although stage 2 telemetry failed 12s after separation from stage 3. A 19m50s burn of the S400 apogee motor at 6th apogee circularized the orbit. Control was swapped every 6 months between GSOC and CNES/Toulouse.
| Symphonie MV1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1974 Dec 19 | 0239:00 | Launch by Delta 2914 | CC LC17 |
| T+0:38 SRM 1-6 out | |||
| T+0:39 SRM 7-9 on | |||
| T+1:17 SRM 7-9 out | |||
| T+1:27 SRM 1-9 sep | |||
| T+3:48 MECO | |||
| T+3:53 VECO | |||
| T+3:56 St 1 sep | |||
| 0243:01 | T+4:01 SES-1 4:49 | ||
| T+4:50 Fairing | |||
| 0247:50 | T+8:50 SECO-1 169 km 7.955km/s0 7 | 170 x 706? x 27.0? | |
| 0303:05 | T+24:05 SES-2 17s 137m/s? 372 km | ||
| 0303:22 | T+24:22 SECO-2 377 km | 284 x 1103 x 27.0 | |
| 0304:16 | T+25:16 St 2 sep | ||
| 0304:56 | T+25:57 TES 44s | ||
| 0305:40 | T+26:40 TECO | ||
| 0306:55 | T+27:54 St 3 sep | ||
| St 3 orbit | 423 x 38250 x 12.6 (est) | ||
| St 3 orbit | 427 x 38194 x 12.7 (Jun 1976) | ||
| 1974 Dec 19 | 0310 | 683.50 405 x 38245 x 13.2 | |
| 1974 Dec 21 | 1715 | Apogee firing 19:50 | 1451.76 34067 x 38119 x 0.56 |
| 1735 | LAM firing complete | ||
| 1974 Dec 23 | 1620 | TCM | 1477.98 35068 x 38136 x 0.65 |
| 1974 Dec 24 | 0700? | Despin via yo-yo | |
| 0700 | Solar panels deployed | ||
| 1974 Dec 24? | 0438 | TCM | 1417.71 35088 x 35918 x 0.47 |
| 1975 Dec 29 | 1530 | TCM | 1427.72 35340 x 35903 x 0.45 |
| 1975 Jan 3 | 0905 | TCM | 1440.72 35783 x 35967 x 0.46 |
| 1975 Jan 6 | 1512 | TCM plane | |
| 1975 Jan 8 | 0313 | TCM | 1440.43 35772 x 35966 x 0.02 |
| 1975 Jan | GEO 11.5W | ||
| 1977 Mar 4 | Mv out | GEO 11.5E | |
| 1977 May 26 | Mv in for STEP project | GEO 49E | |
| 1977 Nov 10 | 1436.21 35781 x 35795 x 0.1 GEO 49.0E | ||
| 1979 Apr 18 | 1436.09 35775 x 35797 x 0.5 GEO 48.7E | ||
| 1979 Jul 3 | Mv out | GEO | |
| 1979 Sep 3 | Arrive on station | GEO 11.5W | |
| 1979 Sep 15 | 1436.04 35771 x 35799 x 0.8 GEO 11.5W | ||
| 1981 Oct 23 | 1435.97 35772 x 35796 x 2.4 GEO 10.6W | ||
| 1982 Aug 19 | 1436.15 35777 x 35798 x 3.1 GEO 11.2W | ||
| 1983 Jul 14 | 1436.13 35782 x 35792 x 3.9 GEO 11.7W | ||
| 1983 Aug 3 | Raise orbit 80km | ||
| 1983 Aug 4 | end of transmissions | ||
| 1984 Nov 23 | 1440.37 35861 x 35878 x 5.0 | ||
| 1989 Dec 23 | 1440.68 35860 x 35891 x 9.5 | ||
| 1992 Jan 5 | 1440.36 35855 x 35884 x 11.1 | ||
| 1995 Jul 5 | 1440.37 35846 x 35894 x 13.4 | ||
| 1998 Sep 14 | 1440.54 35844 x 35902 x 14.6 | ||
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